CHARACTERISTICS AND PERFORMANCE HANDBOOK U.S.S.R. AIRCRAFT

• Document Type: CREST
• Collection: General CIA Records
• Document Number (FOIA) /ESDN (CREST): CIA-RDP81-01043R002000100005-9
• Release Decision: RIPPUB
• Original Classification: S
• Document Page Count: 156
• Document Creation Date: December 23, 2016
• Document Release Date: June 4, 2013
• Sequence Number: 5
• Publication Date: January 1, 1958
• Content Type: REPORT

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CHARACTERISTICS
AND
PERFORMANCE HANDBOO
Assistant Chief of Staff / Intelligence ?
and
Office of Naval Intelligence ? USN
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R
50X1 -HUM
Next 1 Page(s) In Document Denied
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0
AMC Desionation
FLORA
FAGOT
FRESCO
FARMER
FLASHLIGHT A
FLASHLIGHT B
FLASHLIGHT C
FACEPLATE
FISHBED A
FISHBED B
FISHPOT
FITTER
BEAST
BAT
BULL
BARGE
BEAGLE
BOSUN
BADGER
' BISON
BEAR
BLOWLAMP
BACKFIN
CREEK
COLT
CAB
CORK
,COACH
CRATE
CAMEL
CAMP
.CAT
MULE
MOOSE
MAX
January 1958-
SECRET
TABLE OF CONTENTS ,..
USSR Designation
Fighters
Yak-23
Mig-15
Mig-17
Mig-19
Yak-25
Bombers
11-10
Tu-2
Tu-4
11-28
Tu-14
Tu-16
Transports
Yak-12
An-2
Li-2
Yak-16
11-12
-11-14
Tu-104
Trainers
Po-2
Yak-11
Yak-18
SECRET
Date
Sep 55 (C)
Mar 56 (C)
Jun 56 (C)
Oct 57 (S)
Oct 57 (S)
Jan 57 (S)
Jan 57 (S)
Dec 57 (S)
Jan 57 (S)
Jan 57 (S)
Jan 57 (S)
Dec 57 (S)
Jul 53 (C)
Mar 52 (C)
Mar 52 (C)
Jan 54 (C)
Jun 56 (C)
Mar 52 (C)
Dec 57 (S)
Dec 57 (S)
Dec 57 (S)
Nov 56 (S)
Jan 58 (S)
Jul. 53(C)
Jul 53 (C)
Jan 58 (C)
Jul 53 (C)
Jul 53 (C)
Oct 57 (C)
Nov 57 (C)
Sep 57 (C)
Oct 57 (C)
50X1-HUM
Jul 53 (C)
Jul -53 (C)
Jul 56 (C)
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AMC Designation
SECRET
TABLE OF CONTENTS (Cont)
?
USSR Designation Date
Trainers (Cont)
MASCOT UI1-28 Jul 53 (C)
MIDGET UMig-15 Jul 53 (C)
Reconnaissance
MOP GST Jul 53 (C)
MOLE Mar'52 (C)
MADGE Be-6 Jul 52 (C)
Gliders.
MARE,
Mar 52. (C)
Rotary Wing
HARE Mi-1 Jan 58 (C) ,
HOUND Mi-4 Sep 57 (C)
HORSE Yak-24 Jan' 58 (C)
?
50X1-HUM
January 1958
SECRET ?
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CONFIDENTIAL
Septeniber
1955
FLORA (YAK-23)
REMARKS: The YAK-23 (FLORA) is a single seat low-wing light-weight fighter. It is the latest
version of a series of jet fighters designed by YAKOVLEV. Other known aircraft in the series which
began with the YAK-15 are the YAK-17 and UYAK-17.
50X1-H111
SUMMARY
1955 First observed in the July 1948 airshow aircraft is now believed obsolete in Soviet
Air Force.
CONFIDENTIAL
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S
te*.?
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CONFIDENTIAL
FLORA (YAK-23)
September
1.955
DIMENSIONS
WEIGHTS
FUEL
Wing
Span
Area.
L.E. Taper
T.E. Taper
Overall Length
Maximum Diameter
Overall Height
28.5 ft
147 sq ft
11.5 deg
7 deg
26.8 ft
4.7 ft
11.3 ft
Loading
Empty
Take-off
Lb
4400
6600 (w/o external tanks)
7359 (v/external tanks)
Internal
External
Weight, lb
1615
Gal
241
104
POWER PLANT
ENGINE RATINGS
BOMBS/FREIGHT
No. & Model
Type
Length
Diameter
Weight (dry)
(1) RD 500
Centrifugal
93 in
43 in
1414 lbs
SL Static
Max
Nor
Lb
3,470
1,763
RPM
14,700
12,500
NONE
GENERAL INFORMATION
General information only is quoted hereon. For more detailed information
on characteristics and performance see ATIC Technical Report TR-AC-28, entitled
(Unci) Soviet YAK-23 Aircraft.
Retractable tricycle landing gear. Pneumatio system. A mechanical push-pull
system without booster unit is the means of actuating ailerons. Flaps are
pneumatically actuated.
Fuselage 'is of iemi-monocoque construction' and has two detachable sections.
Fuel tanks are located In the fuselage.
Equipped with ejection seat.
Combination "demand" and "free-flow" type oxygen system.
ELECTRONICS
RSI 6K Command Transmitter
RSI-6M-1 Command Receiver
RPKO-10M Radio Compass Receiver
Sch-3M IFF
_
GUNS
2 x 23-mm KR (90 rounds per gun)
ROCKETS
NONE
CONFIDENTIAL
25
4P)
September
1955
CONFIDENTIAL
ailiMIMMINIMM=M
FLORA (YAK-23)
AIRCRAFT
PERFORMANCE
CONDITIONS
MISSION 12
MISSION 23
TAKE-OFF WEIGHT
(lb)
(lb)
(lb)
(psf)
(ho)
(ft)
(ft)
(flan)
(min)
(min)
(ft)
(124)
(124)
(ku)
(ft)
(ft)
(12r)
(lb)
(ft)*
(ho)
(rpm)
(ft)
(ft)
(fpm)
(kn)
(ho)
(1)
(1
(1
(1
(1)
(1)
(1)
(1)
(1)
(1)
(1)
(1)
6,600
1,615
165
45
86
1,345
2,290
9,42o
6.3
8.3
52,000
487
115
360
35,600
35,600
0.95
5,892
35,500
460
4,000
50,600
53,400
10,600
504
360
'
7,297
2,312
165
49.7
86
1,720
2,700
7,900
8.7
11.8
50,000
720
250
360
35,600
35,600
1.58
6,247
35,500
460
2,700
48,500
51,000
9,000
504
360
_
50X1
-HUM
Fuel at 6.7 lb/gal
Payload (ammunition)
Wing loading
Stall speed (power off, clean)
Take-off ground run at SL
Take-off to clear 50 ft
Rate of climb at SL
Time - SL to 35,000 ft
Time -.SL to 40,000 ft
Service ceiling (100 rpm)
COMBAT RANGE
COMBAT RADIUS
Average speed
Initial cruising altitude
Final cruising altitude
Total zaseion time
com2AT WEIGHT
Combat altitude
Combat speed
Combat climb
Combat ceiling (500 fpm)
Service ceiling (100 fpm)
Max rate of climb at SL
Max speed at SL
Basic speed at 35,000 ft
NOTES
* Limited-by no pressurization provisiona and presently installed oxygen equipment
1. Military power
2. HIL-C-5011 Basic Mission
3. MIL-C-5011 with 2 - 52 gal external fuel tanks
50X1 -HUM
CONFIDENTIAL
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CONFIDENTIAL
FLORA (YAK-23)
7
7: 6
25
1
TAKE-OFF
4
FLU
11
It
It
I
I I
I
41.????
7
, ?
I 1,1
8
9
GROSS WEIGHT ( 1000 lb)
10
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September
1955
?
SPEED
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, CONFIDENTIAL
? ?
?
MARCH 1956
CONFIDENTIAL
FAGOT (MIC-15 BIS)
FAGOT with VK-1 Engine
FAGOT with RD-45 Ermine
REMARKS .The 14IG-15 (FAGOT) is a single seat swept-wing turbojet day interceptor. There are two
models; the early 14IG-15, and the 141G-15 His, which is an improved version. Recent examination of both
models has confirmed previous estimates that both models are identical in size, and there are no signi-
ficant external differences. Difference between models is in engine power and electronic equipment.
The early model has a direct copy of the British Rolls-Royce Nene rated at 5,000 lbs thrust at SL.
Max speed of this version is 564 knots and rate of climb is 8300 ft/min at SL: Aircraft are also
produced in Czechoslovakia.
SUMMARY
50X1 -HUM
CONFIDENTIAL
50X1 -HUM
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MARCH 1956
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CONFIDENTIAL
FAGOT (MIG-15 BIS)
DIMENSIONS
Wing
Span
Area
Cathedral
Sweepback (leading
Overall length
Fuselage diameter
33.2 ft
218 sq ft
2.0 deg
edge) 36 deg
33.4 ft
4.75 ft
POWER PLANT
No & Model (1) VK-1
Type Centrifugal, 1 stage
double sided, 9 cans
Length 93.0 inches
Diameter 50.0 inches
Weight (dry) 1980 lbs
Exhaust nozzle diameter 10.67 inchee
Exhaust nozzle area 358 eq in
WEIGHTS
Loading
lb
Empty
8,350
Take-off
11,000
Combat
9,745
Landing (Approx)
8,915
ENGINE RATINGS
SL Static lb RPM SFC
*Take-off 5950 11,500 1.10
lbe/lb/hr
5290 11)200 1.06
4760 10,870 1.05
**Military
Normal
* 5 min rating
** 60 min rating
GENERAL INFORMATION
General information only is quoted hereon. For more detailed information on
characteristics and performance, pee ATIC TR-AC-48, entitled (Uncl) MIG-15 Bia
Flight Test, dated 11 July 1955.
The fuselage has an air intake in the none and jet exhaust in the tail.
Wings have a pronounced sweep-back ending in square tips. Horizontal and vertical
tail surfaces also have a pronounced eweep-back. Horizontal stabilizer in set
high on. the verticil fin. A.prominent feature in the four ridge? (fences) on the
upper surface of the?wing extending from leading edge to trailing edge.
Retractable tricycle landing gear. Hain gear retracta inward into the
wing near the root.
All systeme hydraulically operated except wheel brakes and emergency system
for flaps and undercarriage which are pneumatic.
Electric trim tabs on aileron and elevator.
Pressurized 'and heated cockpit.
Canopy opens from left side of aircraft.
Air brakes are located on either aide of rear fuselage. Spring loaded, push
button on left of control grip enables easy use during engagement or formation
flying.
Defroating in accomplished by warm air preosurization distributary tube.
Under certain humidity conditions and during descent with throttle back, mist
forms on canopy fram front to rear and will not clear until engine has been
operated a short time at max power.
Flight tests revealed the following:
Poor rearward vision.
Aircraft encounters uncontrollable none-up trim change at Mach Number .92.
Aircraft encounters "Dutch Roll" at approximately .84 Mach Number.
FUEL*
Weight, lb Gal
Internal 2,492 372
(2 x 66 gal or 2 x 79 gal external
tanks may be carried)
* Soviet T-1 (similar to JP-1)
BOMBS/FREIGHT
Can carry up to 550 lb bomb from a
shackle under each wing in lieu of
drop tanks
ELECTRONICS
ARK-5 Radio Compass (150-1300 kcs)
RV-2 FM Radio Altimeter (0-1200 meters:
14RP-48P Marker Beacon Receiver (75 me)
SRO-IFF Transponder (157-187 ma)
* RSI-6K Radio Trannmitter
* RSI-6M-1 Radio Receiver (3750-5000
kc)
RSI-U-314 VHF Transmitter-receiver
(100-150 Me)
* This equipment is not carried in
all models.
GUNS
1 x 37 mm N type gun
2 x 23 mm NB type guns
Mounted beneath air intake in front
fuselage
ROCKETS
None ..
?
OX1 -HUM
CONFIDENTIAL
?
MARCH 1956
CONFIDENTIAL
FAGOT (1IG-15 BIS)
AIRCRAFT PERFORMANCE
Basic
Ground
CONDI TIO NS
Mission
Support
AreR Intprepr+
Minginn(P)
TAX-OFF WEIGHT
(lbs)
11,000
12,100
Fuel at 6.7 egal
(lbs)
2,492
2,492
Payload (Ammo)
(lbs)
258
1,100
Wing Loading
(Par)
50
55
.
Stall Speed (Power officlean)
(kn)
116
122
Take-off ground run at SL
(ft)
(1)
1,600
- - .-
Take-off to clear 50 ft
(ft)
(1)
2,600
- . -
Rate of climb at SL
(fpm)
(1)
9,600
8,500
Time - SL to 40,000 ft
(min)
(1)
7.6
- - -
Time - SL to 45,000 ft
(min)
(1)
10.00
. . .
Service ceiling
(ft)
(1)
50,400
49,500
COMBAT RANGE
020
434
435
-
COMBAT RADIUS
(NM)
195
65
Average speed
(lets)
470
535
Initial cruising altitude
(ft)
49,450
25,000
Final cruising altitude
(ft)
52,050
25,000
Total mission time
(hr)
.93
- - -
COMBAT WEIGHT
Os)
9,745
10,100
Combat altitude
(ft)
50,000
SL
Combat speed
(lets)
(1)
504
574
Combat climb
(rpm)
(1)
1,200
10,500
Combat ceiling
(ft)
(1)
51,000
50,500
Service ceiling
(ft)
(1)
52,500
52,000
Maximum R/C at SL
(fpm)
(1)
12,20
10,500
Maximum speed at SL
, (kn)
(1)
583
574
.
Basic speed at 50,000 ft _
(len)
? (1)
504
495
Landing Weight (Approximately) .
(lbs)
8,915
9,000
.
.
NO TES (1) Max Power
(2) Not to Mil-C-5011A
CONFIDENTIAL
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50X1 -HUM
-9
PARCH 1956
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CONFIDENTIAL
TAKE-OFF
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CONFIDENTIAL
12
14
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r.4191' 4-`144'.
CONFIDENTIAL
June
1956
FRESCO
XylogiumiL
a, ammoz.miw.%
A
REMARKS: The MIG-17 (FRESCO) is a single seat swept-wing, turbojet day interceptor. In appear-
ance this aircraft is similar to the MIG-15 (FAGOT) and may be considered a further de-
velopment of that aircraft. There are four versions of this aircraft.
50X1-HUM
SUMMARY
1955 First observed at an air show in Moscow on 23 August 1953. Aircraft is in operational
use in the Soviet Air Force. Small numbers are now being introduced in the satellite
Air. Forces.
CONFIDENTIAL
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50X1-HUM
FRESCO
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CONFIDENTIAL
September
1955
DIMENSIONS
WEIGHTS
FUEL
Wing
BP=
Area
Aspect ratio
32 ft
230 sq ft
4.4
Loading
Empty
Take-off
Combat
Lb
8,545
12,500
11,050
Weight, lb Gal
Internal 2940 440
External 21o?
Cathedral (approx)
2 deg
Landing (approx)
10,050
Sweepbatk
AMPR
6,000
Inboard leading edge
49 deg
Outboard leading edge
43 deg
Overall length
36 ft
Fuselage Diameter
4.73 ft
POWER PLANT
No. di Model
Type
Length
Diameter
Weight (dry)
Exhaust Nozzle
* With afterburner
(1)VI-14.
Centrifugal
93 in.
* 188 in.
30 in.
2010 lb.
* 2360 lb
338 sq in
* 450
ENGINE RATINGS
SL Static
lb
RPM
*
Max
8400
11,500
Military
7000
11,300
Normal
3600
10,870
* With afterburner
GENERAL INFORMATION
General information only is quoted hereon. For more detailed information on
characteristics and performance see ATIO Study No. 102-A0-33/3-34, entitled (Unci)
Analysis of FRESCO.
Aeronautical equipment in FRESCO "A", "B", "0", and "D", versions is
basically identical as that in FAGOT.
Improved instruments (flight and engine), safety equipment (ejection seat,
wait provisions, etc.,) will be found in Fusco.
Identification features common to all FRESCO versions are:
a. There is a break in tbs wing leading edge at approximately semi-span
positien, three tall fences are located on each wing.
b. Two pitot static heads are on each wing tip.
c. Rear fuselage bee smooth fairing to tail and there is a ventral fin
on underside of fuselage which may also serve as tall bump.
d. There is a protrusion on top of canopy.
Identification features not common tt. all versions are:
FRESCO "A" - Dive brakes aft. (See Figure 1)
FRESCO "B" - Dive brakes aft of wing trailing edge. (See Figure 2)
FRESCO '0' Dive brakes aft and tailpipe protruding from fairing.
(See Figure 3)
FRESCO "D" - Same as "On model with the addition of a Radome on upper
surface of the air intake similar to U. S. 1,-86D. Also
there appears to be a redone in the air intake island.
NOTE: Dive brakes are larger than those on the FAGOT.
2 x 105 gal drop tanks under wings
pylon mounted.
I BOMBS/FREIGHT
Bombe can probably be carried in
multipurpose pylon.
ELECTRONICS
ARK-5 Radio Compass (150-1300KCS)
RV-2 FM Radio Altimeter (0-1200
meters)
m55p-48p Marker Beacon Receiver (75 C)
SRO-IFF Transponder (157-187 )C)
RSI-6K Radio Transmitter
28I-68-1 Radio Receiver (3750-5000 KC)
RSI-U-3M VHF Transmitter-Receiver
(100-150 MC)
Range only radsr
FRESCO "D" (only)
Search and Track Al/Fire Control 'WAX
GUNS
1 x 37 mm N Type gun
2 x 23 rm UR Type guns
ROCKETS
NONE
CONFIDENTIAL
CONFIDENTIAL
September
1955
FRESCO A & B
AIRCRAFT
PERFORMANCE
CONDITIONS
Area
Intercept
Area
Intercept(2;
Optimum
Miesion (2)
TAKE-OFF WEIGHT
(lb)
(lb)
(lb)
(Pe)
(knots)
(ft)
(ft)
(fpm)
(min) .
(min)
(ft)
(x04)
(Km)
(mote)
(ft)
(ft)
(hr)
(1
(ft)
1
(knots)
(Ppm)
(ft)
(ft)
(rpm)
(knots)
(knots)
(lb)
(1)
g3
(1)
(1)
(1)
(1)
(1)
(1)
(1)
(1)
(1)
(1)
12,500
2,940
270
50
115
1,4601,860
2,64.
12, 200
6.3
9.4
53,900
625
280
510
49,300
52,600
1.20
11,145
50,000
540
1,800
54,800
56,500
13,900
620
540
10,000
105
14,085
4,345
270
56
120
3,2.4.
9,900
7.6
14.1
50,800
1,180
565
510
46,700
52,500
2.32
11,780
50,000
540
1,600
53,700
54,800
13,050
620
540
10,100
105
14,085
4,345
270
56
120
1,860
3,140
9,900
7.6
14.1
50,800
1,400
610
510
46,700
53,700
2.48
11,670
50,000
540
1,700
53,900
55,400
13,200
620
540
9,860
105
.
.
Fuel, at 6.7 lb/gal
Payload (Ammunition)
Wing loading
Stall speed (power off, clean)
Take-off ground run at SL
Take-off to clear 50 ft
Rate of Climb at SL
Time - SL to 40,000 ft
Time - SL to 50,000 ft
Service ceiling (100 fpm)
COMBAT RANGE
COMBAT RADIUS
Average speed
Initial cruising altitude
Final cruising altitude
Total miesion time
COMBAT WEIGHT
Combat altitude
Combat speed
Combat climb
Combat ceiling (500 fpm)
Service ceiling (100 rpm)
Max rate of climb at SL
Max opeed at SL
Basic speed at 50,000 ft
LANDING WEIGHT (Approximate)
Stall speed (clean)
' .
,
NOTES 1. military pover
2. With extersal fuel
50X1-HUM
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
CONFIDENTIAL
50X1-HUM
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
FRESCO C & D
CONFIDENTIAL
September
1955
CONFIDENTIAL
September
1955
AIRCRAFT PERFORMANCE
TAKE-OFF
SPEED
CONDITIONS
Area
Intercept
Area
Intercept
Ground
Attack (2)
DISTANCE
(1000 ft)
ALTITUDE
(1000 ft)
TAKE-OFF WEIGHT
Fuel at 6.7 lb/gal
Payload Ammunition
Wing loading
Stall speed (power off, clean)
Take-off ground run at SL
Take-off to clear 50 ft
Rate of Climb at SL
Tine - SL to 40,000 ft
Time - SL to 50,000 ft
Service ceiling (100 fpm)
COMBAT RANGE
COMBAT RADIUS
Average Lspeed
Initial cruiping altitude
Final cruising altitude
Total mission time
COMBAT WEIGHT
Combat altitude
Combat speed
Combat climb
Combat ceiling (500 fpm)
Service ceiling (100 fpm)
Max rate of climb at SL
Max speed at SL
Basic speed at 50,000 ft
LANDING WEIGHT (Approximate)
Stall speed (clean)
(lb)
(lb)
(lb)
(pal)
(knots)
(ft)
(ft)
(rpm)
(min)
(min)
(ft)
(NM)
(NM)
(knots)
(ft)
(ft)
(hr)
(lb)
(ft)
(knots)
(fpm)
(ft)
(ft)
(Ppm)
(knots)
(knots)
(lb)
(kts)
MAXIMUM POWER
--- MILITARY POWER
EUMM::::MUMM MEM
IMEMMMOMM: :::::1"M"
? ISM MUNS:::::::
57,500
520
MMUMMERAMMMEllal
? MAXIMUM POWER
--- MILITARY POWER
11,050 LB
510
47,100
52,500
1.91
500
510
47,100
53,700
2.13
?
?
CiVISUP--.??kg
^WMMEM.r.NON1111
im5 om. inhaamPrriammu"?
ammap.173,,minali
MANUS"
.. -"
GROUND RUN
480 520 560 600 640
GROSS WEIGHT ( 1000 ib)
TURN RADIUS
CLIMB
RADIUS OF TURN
1000 ft)
45
Fresco "D" altitude capability will be decreased approximately
300 feet due to the 200 pound increase in take-off weight.
40
35
30
25
20
15
10
ALTITUDE
(1000 ft)
LEVEL FLIGHT
DIVING FLIGHT
FF,050 LB (CLEAN) -
55,000 FT
T/G 12,500
LB @ 0 ?TIC 12,500
mri
LB @ T.O.
211111111111111110111IIIMPIL
lik3111 11111111111111111111
III
oiiii,iijigooii
111111410i01111111
MAXIMUM POWER
MILITARY POWER
WEIGHT REDUCTION DURING
GROUND OPERATION AND
CLIMB CONSIDERED UNLESS
OTHERWISE NOTED.
ma ma iiimititt
R/C 12,500
LB TO
IMUM ?
EMMUIMILIBM
MESIINMVVEMMIT: mmmmmmmm '1,-.0111g;
MIMS
t!!!!!!
'UMW
mmmmmm 7:1111WWEIBM
MIL,KIMMO
MEWILIMM
Ii LB -Cr. a
.6 .8 .9
MACH NUMBER
R/C 12,500
LBS (CONST)
1 'film
16 18
6 8 10 12 14
TIME TO CLIMB -MIN
1 I i 1 1 1 i 1
4000 12,000 20,000 28,000 36,000
RATE OF CLIMB-FT/MEN'
NOTES 1. Max power.
2. No distance credit for 2 min NRP SL, 1 min Max Powcr@ SL, 2 MP IS SL, 1 min Max Power SL,
15 min loiter @ SL.
3. Saam as Area Intercept except that reserve is fuel required for 10 minutes loiter at SL.
CONFIDENTIAL
CONFIDENTIAL
50X1 -HUM
50X1 -HUM
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
.O..1.165.0.11148.15:14.12L
October
1 1957
j
SECRET
FARMER
REMARKS: FARMER is a single place twin-engine high performance day interceptor.
First observed during rehearsal for May Day 1955 Air Show.
SECRET
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
SECRET
FARMER
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
OCTOBER
1957
DIMENSIONS
Wing
Span 32 ft
Area 305 sq ft
Sweepback leading edge 56 deg
Overall length 42 ft (48.45 w/boom)
Maximum depth (fUs) 4.75 ft
width 5.4 ft
Tail
Span 17 ft
Sweep 56 deg
VT Height above fuselage
centerline 7.5 ft
, POWER PLANT
No. & Model
. Type
Length
Diameter
Weight (dry)
(2)
Axial-flow turbojet
160 inches
27.5 inches
1830 lbs with A/B
WEIGHT
Loading
lb
Empty
12,340
Take-off
17,300
Combat
15,400
Landing (aprx)
13,970
ENGINE RATINGS
SL Static
Max
Mil
lb SFC/#/hr/#
6700 1.85
5000 0.935
GENERAL INFORMATION
Single place day fighter.
Tricycle landing gear.
:Bubble canopy. '
Range only radar of the US AN/APO-30 type to provide range input to gyro lead
computing gunsigbt.
FARMER has been observed carrying 2 x 210 US gal drop tanks.
Soviet designation of FARMER is MIG-19.
FUEL
Internal
External
Weight, lb Gallons
14000 600
2800 420
BOMBS/FREIGHT
Probably capable of carrying one
500 Kg (1100 lb) bomb on each wing.
ELECTRONICS
Radar
Range only
IFF - SRO (157-187 Mc)
Navigation
Radio compass - ARK-5
Radio altimeter, low - RV-2
Marker beacon receiver - MRP-48P
Communications
VHF command radio, 4-channel -
RSIU-3M ?
' (3 li N :3 .
,
Forward firing guns 2 x 23 with cyclic
rate of 800-900 rds/min and one
improved N-37 with cyclic rate of
475-525 rds/min. Ammunition storage
for 6 sec fire.
C
ROCK ET :3
Capable of carrying one large caliber
multiple missile warhead rocket or Up
to 40 small caliber rockets in a '
honeycomb type pod, under each wing.
OX1-HUM
SECRET
-
?
?
SECRET
OCTOBER
1957
FARMER
AIRCRAFT
PERFORMANCE
CONDITIONS
Area (4)
Intercept
Basic Mission
Area
Intercept
Mission
Area (4)
Intercept
Opt. Mission
Area
Intercept
Opt. Mission
TAKE-OFF WEIGHT
(lb)
,Basic
20,500
17,300
20,500
17,300
Fuel at 6.7 lb/gal
(lb)
6,800
4,000
6,800
4,000
Payload (Ammo)
(lb)
270
270
270
270
Wing loading
(Per)
67
57
67
57
Stall speed (power off, clean)
(kts) ,
135
130
135
130
Take-off ground run at SL
(ft) (1)
1,700
1,200
1,700
1,200
Take-off to clear 50 ft
(ft) (1)
3,000
2,200
3,000
2,200
Rate of climb at SL
(fpm) (1)
10,000(6)
39,500
10,000(6)
39,500
Time - SL to 40,000 ft
(min) (1)
(2)
(3)
7.9(6)
2.6
7.9(6)
2.6
Time - SL to 50,000 ft
(min) (1)
(2)
(3)
---
3.9
---
3.9
Service ceiling (100 fpm)
(ft) (1)
(2)
53,800
59,400
53,800
59,400
COMBAT RANGE
(NM)
1,285
--
1,475
695
COMBAT RADIUS
(NM)
565
180
655
245
Average speed
(kts)
535
540
535
540
Initial cruising altitude
(ft)
43,900
51,200
43,900
51,200
Final cruising altitude
(ft)
49,900
53,700
54,300
54,300
Total mission time
(hr)
2.22
.82
2.56
.94
COMBAT WEIGHT
(lb)
(5)
16,600(17,000)
15,400
16,300(16,700)
15,200
Combat altitude
(ft)
50,000
50,000
50,000
50,000
Combat speed
(kts) (1)
(5)
630(565)
640
630(560)
645
Combat climb
(fm) (1)
4,800
5,600
4,900
5,700
. Combat ceiling (500 fpm)
(ft) (1)
(5)
59,300(56,300)
60,900
59,700(56,700)
61,100
Service ceiling (100 fpm)
(ft) (1)
.
60,500
61,900
60,800
62,200
Max rate of climb at SL
(fpm) (1)
41,200 -
44,700
42,000
45,200
Max speed at SL
(kts) (1)
680
680
680
680
Max speed at optimum altitude
(kt8/ft)(1)
710/35,000
710/35,000
710/35,000
710/35,000
Max mach number at optimum altitude
(mn/ft)(1)
1.24/35,000
1.24/35,000
1.24/35,000
1.24/35,000
-
-
(1)
NOTES (2)
(3)
(4)
(5)
(6)
Maximum power.
Allows for weight reduction during ground operation and climb.
Includes 0.8 min for take-off and acceleration to climb speed without tanks 'or 0.9 .50X1 -HUM
With 2 x 210 U. S. gal tanks. .
Numbers in parenthesis are for aircraft with empty tanks aboard.
Military power.
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
SECRET
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
TAKE-OFF
DISTANCE
(1000 FT)
SECRET
111111111111
NUNI
?
MEM
MMUIMMIERMINOMMEMOMME
--I-
U...
M^ MMMMM MEM
^ MMMMM MMUMMUNIONMAIS
?11?NMAINIliall?
lal"."11114161"113??????trgrrOMMINFIlliMm
Mr1111111.11.1.11...1.1""FIN?S?JC:????111111M111101MEN?
,1"911":=1.1"'
.1111181:111?11E'
GROUND RUN
0
14
16
18
GROSS WEIGHT (1000 LB)
20
ALTITUDE
(1000 FT)
70
60
50
40
30
20
10
0
OCTOBER
1957
CLIMB
M ?
IIIIIIIIIIIIIII 111:91:11"m I"; ::!
KARSIMMMOMMMEROMMOM MIN
TIC
? MAX PWR
----- MIL PWR
? 17,300 LBS
(a)
ma?tam
T.O.
3111111 i/1111111111111111 III
lig1111111111111Wili- 1111111111111 III
MNUM^ EM:411:gil:
1::::=11k4111
WEIGHT REDUCTION DURING :
GROUND OPERATION AND CLIMB
CONSIDERED UNLESS
OTHERWISE NOTED
IIIISKIMENII
ni!
.^ ..m.Kmo MMMMM 11.104116 IMMISIIMEMNSUMEM
MIRMagararnilaMitnOtIMMEMMUMEM
rpi71.11142 OMMUMINIM
^ourAsammayeamantili
MlWAMMINNE NMI aabillEG
INUIRM MMMMMM e:: RIG trit0:141
WWI
:I:a 17,300 LBS IntitiM MMMMM um
IEM?I (CONSTANT) Ill
WM11111111 a on I 1 Ilmmliiiiii1111111
10,000 20,000 30,000 40,1000
RATE OF CLIMB-FT/MIN
RIC
17,300 LBS
@T.O.
2 4 6
TIME TO CLIMB-MIN
113
ALTITUDE
(1000 FT)
70
60
50
40
30
20
10
SPEED
? MAX PWR
--- MIL PWR
.1
-
Gw=15,400LB
tflIJIIII11111
COMBAT WT 17,000 LB
II
mum
ri?Ton
?....
sown
Erman
IrA I
MIN Nar
ANL
PS 11
0
540 580
Ii
W/ TANKS
II
620
KNOTS
660 700
ALTITUDE
(1000 FT)
10
8
6
4
TURN RADIUS
I.
?
MUMMOMMIIIIM
SECRET
II
UIU
?
? LEVEL FLI HT
----- DIVING ELI HT
1
?
GW=15,400 LB _
?
?
?
?
?
II
?
?
?
al
MI
45,000 FT
1 11
111
35,000 FT
7 .8
411
tsSomp
MACH NUMBER
.9
1.0
50X1 -HUM
(11
SECRET
October
1957
FLASHLIGHT A
REMARKS
? ? FLASHLIGHT is a two place twin jet swept wing all weather fighter.
SUMMARY '
1955 First observed during rehearsals for May Day 1955 airshow. It is in operational
units.
SECRET
50X1 -HUM
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
?
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
SECRET
FLASHLIGHT A
OCTOBER
1957
DIMENSIONS
Wing
Span
Area
Sweepback puce
Overall length
Max diameter (fus)
Nacelle diameter 3
Nacelle length
Tail
Span
Sweep
Height from fuselage
center line
*Inboard leading edge
36 ft
' 300 sq ft
47 deg
50.7 ft
4.75 ft
x 2.63 ft
15 ft
13 ft
45 deg
9.6 ft
POWER PLANT
No. & Model
Type
Length
Diameter
Weight (dry)
(2)
Axial-flow turbojet
110 inches
27.5 inches
1480 lbs
WEIGHTS
Loading
lb
Empty
13,640
Take-off
20,200
Combat
17,900
Landing,(aprx)
16,000
AMPR
10,000
ENGINE RATINGS
SL Static
lb SFC/#/hr/#
Max 5100 .92
GENERAL INFORMATION
Two place all-weather fighter.
Landing gear is tandem type with the main gear carrying approximately 9c4 of
the weight.
All-weather armament system incorporating Al search and fire control radar and
computing equipment to provide e capability for lead pursuit attacks under day,
night, and all-weather condition. Such a system should give a long range search,
track and operational capability equivalent to the USAF E-1 Armament System.
FLASHLIGHT A has been observed carrying a ventral tank.
Soviet designation of FLASHLIGHT A is YAK-25.
FUEL
Internal
External
Weight, lb Gallons
5100 760
900 132
BOMBS/FREIGHT
None
ELECTRONICS
Radar
Al
IFF - SRO (157 - 187 Mc)
Navigation
Radio compass - ARK-5
Radio Altimeter, low - RV-2
Marker beacon receiver - MRP-48P
Communications
VHF Command radio - 4 channel -
RSIU-3M
GUNS
2 x 37 N or improved N guns with a
cyclic rate of 400-525 rds/min and
sufficient ammunition for 6 sec of
fire.
5(
ROCKETS ,
Rockets can be carried externally.
-
Xl-HUM
SECRET
?
SECRET
OCTOBER
1957
FLASHLIGHT A
AIRCRAFT
PERFORMANCE
CONDITIONS
Area (4)
Intercept
Basic Mission
Area
Intercept
Basic Mission
Area (4)
Intercept
Opt. Mission
Area
Intercept
Opt. Mission
TAKE-OFF WEIGHT
(lb)
21,200
20,200
21,200
20,200
Fuel at 6.7 lb/gal
(lb)
6,000
5,100
6,000
5,100
Payload (Ammo)
(lb)
300
300
300
300
Stall speed (power off, clean)
(kts)
155
150
155
150
Take-off ground run at SL
(ft) (1)
2,900
2500
2,900
2500
Take-off to clear 50 ft
(rt) (1)
4,60o
4200
4,600
4200
Rate of climb at SL
(fPcs) (1)
9,800
10,800
9,800
10,800
Time: SL to 40,000 ft
(min) (1)(2)
(3)
8.4
7.8
8.4
7.8
Time: SL to 45,000 ft
(min) (1)(2)
(3)
11.8
11.5
11.8
11.5
Service ceiling (100 fn)
(ft) (1)(2)
46,800
48,100
46,800
48,1oo
Wing loading
(Psf)
71
68
71
68
COMBAT RANGE
(NM)
950
805
1,100
945
COPLBAT RADIUS
(1124)
455
380
530
450
Average speed
(kts)
500
500
500
500
Initial cruising altitude
(ft)
45,300
46,300
45,300
46,300
Final cruising altitude
(ft)
49,200
49,600
49,800
50,200
Total mission time
(hr)
(3)
1.92
1.66
2.22
1.93
COMBAT WEIGHT
(lb)
18,400
17,900
18,100
17,600
Combat altitude
(ft)
48,300
49,000
48,700
49,300
Combat speed
(kts) (1)
510
515
510
515
Combat climb
(fin) (1)
500
500
500
500
Combat ceiling (500 fpm)
(ft) (1)
48,300
49,000
48,700
49,300
Service ceiling (100 fpm)
(ft) (1)
49,800
50,500
50,200
50,800
Maxima R/C at SL '
(fpm) (1)
11,300
12,200
11,600
. 12,400
Maximum speed at SL
(kts) (1)
605
-
610
605
610
Basic speed at 35,000 ft
(kts) (1)
540
' 540
540
540
Max Mach number at opt, altitude
(mn/ft)(1)
'
.94/35,000
.94/35,000
'
L_IOTES
(1)
(2)
(3)
(4)
Maximum power.
Allows for weight reduction during ground operation and climb.
Includes 1.4 minutes for take-off and acceleration to climb speed.
132 U. S. gal ventral tanks. '
50X1 -HUM
111?1???????
SECRET
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 ? CIA RDP81 01043R00 0 on
-
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
FLASHLIGHT A
i Ili T
1
i . 1
E
: 1-1 ININA N.- ' '
lilifilillni 111111111111111 _ -
MUM -,- t.? .- ..::11 '4. - --Ff.
IIM
FP-Mann I CLEAR SO FT 1-_-
--:
rIppatIMEIZIERNIM
IIIMPLaggiilmillERVIREI
eiNEEZIEZI 121ErarIP?' '
-1-1-
.1 _t_.?:.
ALTITUDE
(1000 FT)
WEIGHT REDUCTION DURING
-I GROUND OPERATION AND CLIMB
H CONSIDERED UNLESS NOTED50 -
?1 1
T/C 20,200 LB @T.O.
J44..4
RIG
17,900 LB
-4-- (CONST) -
.-....__I-.. . 1 ? ...--.1,...-..-1--1--1.-1.-i-,..-.
7 Vc-SPEED FOR BEST CLIMB
.:::. Vs-STALL SPEED CLEAN 'COND
....-.T.Tfa. r1gran
_ Vs COMBAT WT IfiririTallouum
-
17900 LB
111111111COMBAT
-
:20,200 LB, LA
r
! .
, _ LEVEL FLIGHT _t
17,900 LBS " ? DIVING FLIGHT
REMARKS: FLASHLIGHT B is a plexiglass nose variant of the FLASHLIGHT C. The avant' purpose of
the aircraft is not known although configuration appears suitable for attack or reconnaissance role.
=A:7
tr-'-' Et:ET 11'11.---r.4.
.77?1g
? MAX POWER
-- NORM POWER. .2!E
? ROA !gilt-HTFlr]
First observed during the June 1956 Tushino Air Display.
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
SECRET
FLASHLIGHT B
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
January
1957
DIMENSIONS
Wing
Span
Area
Sweepback THU*
Sweepbatk ORLI**
Overall length
Max diameter (ft.)
Tail
Span
Sweep
Height from fuselage
center line
*Inboard leading edge
**Outboard leading edge
36 ft
305 sq ft
57.5 deg
44 deg
54.75 ft
1..75 ft
13 ft
51 deg
9.6 ft
POWER PLANT
So & Model
Type
Length
Diameter
Weight (dry)
(2)
Axial flow turbojet
160 inches
47.5 inches
1830 lbs
WEIGHTS
Loading (Attack)
Empty
Take-off
Combat
Landing, aprx
AMER
lb
14,600
23,400
19,100
17,300
10,500
Loading (Reconnaissance) lb
Empty
Take-off
Combat
Landing
AMER
14,400
21,000
18,400
17,100
10,300
ENGINE RATINGS
SL Static
Max
Mil
lb SFC/#/hr/i
6700 1.85
5000 .935
GENERAL INFORMATION
Two place attack/reconnaissance fighter.
Lauding gear is tandaa type with outrigger gear.
On FLASHLIGHT B a plexiglass nose has been added replacing the solid nose on
FLASHLIGHT C .
The bombing navigation radar of the WJSKRCKSI type has been added.
Bomb, or stores may be carried internally.
Special aircraft may be fitted with electronic countermeasure equip:exit.
FUEL
Internal
Weight, lb gal
5100 761
BOMBS/FREIGHT
*Boabs can be carried on estimated 4
external (2/ving). suspension points
Size limited only by allowable weight
for aircraft performance.
*Attack Only
ELECTRONICS
Radar
Bombing navigation MUSHROOM type
IFF SRO typo
Navigation
Radio altimeter, low - 1W:2
Radio compass ARK-5
Marker beacon receiver MRF-48P
*Short range SHOHHEALK
Long range navigation system (MOON)
Distance measuring equipment SD-1
Communication
Esiu-31i (4 channel)
Intercom SPU
*Special mission aircraft only.
GUNS
None
5(
ROCKETS
Alternate load in lieu of bombs:
76 x 55 um FEAR in 4 external pods
(2 it each wing)
ort
4 x 325 um SCATTERHEADS
Xl-HUM
SECRET
SECRET
January
1957
FLASBLIGHT B
AIRCRAFT PERFORMANCE
CONDITIONS
_
Ground Attack
Opt. Mission
.
TAXI-OFF WIGHT
(lb)
23,400
Fuel at 6.7 lb/gal
(lb)
5,100
Payload (Bombs)
(lb)
2,200
_
--- -
Wing loading
(Psf)
76
Stall speed (power off, clean)
(kts)
' 158
Take-off ground run at SL
(ft) (1)
2,500
Take-off to clear 50 ft
(ft) (1)
4,300
Rate of climb at SL
(flo)(1)
20,900
Time - SL to 40,000 ft
(sin)( (2)(3)(4)
.10.1
Time - SL to 45,000 ft
(min) (2)(3)(4)
17.1
Service ceiling (103 fpm)
(ft) (1)
50,300
CCOOLLT RAN3!
(SI)
---
COMBAT RADIUS
(Am)
160
Average speed
(kts)
505
Initial cruising altitude
(ft)
42,300
Final cruising altitude
(ft)
47,300
Total mission time
(hr)
.7
GMAT WIGHT
(1b)
19,100
Combat altitude
(ft)
SL
Combat speed
(kts)(1)
635
Combat climb
(fpm)(1)
26,000
Combat ceiling (500 4a)
(rt) (1)
53,900
Service ceiling (100 fps)
(ft) (1)
54,800
Max rate of climb at SL
(r)(1)
26,000
Max speed at SL
(kts)(1)
635
Max speed at opt. altitude
(kts/ft)(1)
635/SL
.
Max mach number at opt. altitude
(Mn/ft) (1)
1.0/35,000
. .
-
_
NOTES
(1) Maximum power.
(2) Military power.
(3) Allows for weight reduction during ground operation and climb.
(4) Includes 1.0 min. for take-off and acceleration to climb speed.
50X1 -HUM
SECRET
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 ? CIA RDP8 -0
FLASHLIGHTS
111?1???[..
SECRET
Declassified in Part- Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
January
1957
AIRCRAFT PERFORMANCE
CONDITIONS
Reconnaissanc
Basic Mission
Reconnaissance
Opt. Mission
TAKE-077 GROSS WEIGHT
(lb)
21,000
21,000
Fuel at 6.7 lb/gal
(lb)
5,100
5,100
Payload (Ammo)
(lb)
300
500
Wing loading
(lb/sqft)
68
68
Stall speed (power off, clean)
(kts)
150
150
Take-off ground run at SL
(ft) (2)
2,900
2,900
Take-off to clear 50 ft
(ft) (2)
4,6o0
4,600
Rate of Climb at SL
(fP0)(1)
23,400 ?
'23,400
Time: SI. to 4o,000 ft
(min) (2)
(4)(5)
8.6
8.6
Time: SL to 45,000 ft
(min) (2)
(4)(5)
13.8
13.8
Service ceiling (100 fpa)
(ft) (1)
52,900
52,900
COMSAT RAPES
(AM)
595
735
CCKBAT RADIUS
(EM)
300
360
Average speed
(kts)
505
505
Initial cruising altitude
(ft)
114,500
44,500
Reconnaissance speed run
(kts)
(3)
515
515
Reconnaissance altitude
(ft)
45,000
45,300
Final cruising altitude
(ft)
47,300
47,900
Total Mission time ,
(lir)
1.22
1.49
CCUSAT WEIGYX
(lb)
18,400
18,100
Combat altitude
(ft)
45,000
45,300
-Combat speed
(kts)(1)
565
565
Combat climb
(f)(1)
4,800
4,800
Combat ceiling (500 fpa)
(ft) (1)
-54,700
55,000
Service ceiling (100 fro) .
(ft) (1)
55,600
55,900
Max rate of climb at SL
(f1x11)(1)
27,100
27,500
Max speed at opt. altitude
(kts/ft)(1)
635/SL
635/SL
Max each number at opt. altitude
(Mn/ft) (1)
1.0/35,000
1.0/35,000
NOTES Maximum power.
2) Military paver.
(3) Normal power.
(4) Allows for weight reduction during ground operation and climb.
(5) ,Includes 1.0 min. for take-off and acceleration to climb speed.
OX1 -HUM
SECRET
at)
January
1.957
SECRET
FLASHLIGHT B
DISTANCE
(1000 ft)
6
3
2
RECONNAISSANCE VERSION
TAKE-OFF
i..
POWER
MAX POWER
f -
.3: -11...r :47
--OVER SOFT
?
a
..7
-4:
?
?
i?
GROUND RUN
El
sitta-11?11 IIJF
11
=
16 17 18 19 20 21 22 23 24 25
GROSS WEIGHT (1000 lb)
ALTITUDE
(1000 ft)
60
PE ED
_
GW- 18,400 LB !,*--
9iSIS
50
SF-f: TT-N.9:- ?
40
=
d-?
E:55 -rif III IF
30 ffli-it ,-. : 744
Si: !in
,F?,ifti
TU.
II
FI-7, iIi
?L
;!-
74r,
. ?
F4 T., ?
20 agf-i r41111,1 44-4- FIRP. ?
10
1
FI
!Fr. t? Efi,
SL
FAI-1=1-r-=-:-: TF1 II I-F-91E
ri4-.
34
IF.
tjail,11
1111.51
ii it;
500 540
580 620
KNOTS
660
ALTITUDE
(1000 It)
60
50
40
30
20
10
SL
CLIMB
is
FS. 7.4
at;
MAX
MAX POWER
-t---MIL POWER
- -7 -
aar-
-IT/C 21,000 LB AT T. .
=ES
k igE
--:: lAgiffila
MiigEr,-?
talEPI
1 ra
,__ -:._, : -:= _-...-it-z. .
--
'-'-=- -,--_,
-'=21V-7=11
,i21:ii-: -.J 11
I8,400 LB (CORSI)
(CONSINPA:,,,1_,.,71111
T):
1"ril
Eir4.-r:I. F-IMIZtit:
iitlfs
WEIGHT REDUCTION DURING
GROUND OPERAT ON AND
CLIMB CONSIDERED UNLESS
OTHERWISE NOTED
*-
ttO
mat
fiL-4;-1L;
21,000LB
. AT TO. il
iq
4 8 12 16 20 24 28 32 36
TIME TO CLIMB-MIN
1 1 1 1 1 I 1
4 8 12 16 20 24 28 32 36
RATE OF CLIMB
( 1000 FPM I
SECRET
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 ? CIA-RDP81-01043R002000100005 9
50X1 -HUM
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
SECRET
FLASHLIGHT C
REMARKS: FLASHLIGHT C is a two-place twin-jet swept-ving all-weather fighter. It is a
further development of FLASHLIGHT A.
SUMMARY
First observed during the June 1956 Tushino Air Display.
50X1 -HUM
SECRET
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SECRET
FLASHLIGHT C
January
1957
DIMENSIONS
Wing
Span
Area
Sweepback ULE*
Sweepbadk OB1X**
Overall length
Max diameter (tug)
Tail
Spam
Sweep
Height fras fuselage
center line
*Inboard leading edge
**Outboard leading edge
36 ft
305 sq ft
57.5 deg
14 deg
54.75 ft
4.75 ft
13 ft
51 deg
9.6 ft
POWER PLANT
No & Model
T734
Length
Diameter
Weight (dry)
(2)
Aaial flow turbojet
160 inches
27.5 inches
1830 lbs
WEIGHTS
Loading
Empty
Take-off
Combat
Landing, aprx
NOR
lb
14,400
21,000
18,600
16,800
10,300
ENGINE RATINGS
EL Static
Max
Nil
lb SFC/f/hr/it
6700 1.85
5000 .935
GENERAL INFORMATION
Two place all-weather fighter.
Landing gear is tandem type with outrigger gear.
On FLASHLIGHT C the nose Nis been modified to anogiveshape, replacing blunt
nose on FLASHLIGHT A , and afterburners have been added to the engine to give
improved performance.
FUEL
Internal
Weight, lb gal
5100 761
BOMBS/FREIGHT
No bomb load anticipated in 'flew of
interceptor role.
ELECTRONICS
Radar
AI PD-6 w/computer
IFF SRO type
Radar warning receiver
Navigation
Radio compass - ARK-5
Radio altimeter, low - RV-2
Marker beacon receiver - MRP-48P
Communications
VHF 22I0-3m (4 channels)
Intercom SPU type
GUNS
2 x 37 mm N or improved N guns
50 rts/gun. 6 seconds of fire.
50X1
ROCKETS
76 x 55 am FFAR in 4 external pods
(2 in each wing)
OR
4 x 325 mm SCATTERHEADS
OR
Type AAM-1 missiles
-HUM
SECRET
ors
January
3.957
SECRET
FLASHLIGHT C
AIRCRAFT PERFORMANCE
Area
Area
CONDITIONS
Intercept
Basic Missign
0oIllf::en
TA3E-077 WEIGWr (lb)
21,660
21,000
Fuel at 6.7 lb/gal (lb)
5,100
5,100
Payload (Ammo) (lb)
300
300
Wing loading (Pe)
68
68
Stall speed (power off, clean) (kts)
150
150
Take-off ground run at SL (ft)
2,900
2,900
Take-off to clear 50 ft (ft)
4,600 -
4,600
Rate of climb at EL (TA) (1)
23,400
23,400
Time - EL to 40,000 ft (min) (2)(3)(4)
8.6
8.6
Time - SL to 45,000 ft (min) (2)(3)(4)
13.8
13.8
Service ceiling (100 fiml) (ft) (1)
52,900
52,900
COMBAT RAM! (20)
595
735
COMBAT RADIUS (NM)
235
295
Average speed (kts)
505
505
Initial cruising altitude (ft)
44,500
44,500
Final cruising altitude (ft)
47,300
47,900
Total mission time (hr)
---
---
COMBAT WEIGHT (lb)
18,600
18,400
Combat altitude (ft)
50,000
50,000
Combat speed (kts) (1),
560
560
Combat climb (fpm) (1)
2,400
2,500
Combat ceiling (500Cfpm) (ft) (1).
54,400
54,700
Service ceiling (100 fpm) (ft) (1)
55,300
.
55,600
Max rate of climb at SL (fpm) (1)
26,700
27,100
?
Max speed at SL(kts) (1)
635
635
Max speed at opt. altitude (kts/ft)(1)
635/SL
.
635/SL '
Max mach number at opt. altitude (Mn/f)(1)
1.0/35,000
?
1.0/35,000
[NOTES
MexAmum power.
2) Military power.
(3) Alloys for weight reduction during ground operation and climb.
(4) Includes 1.0 min. for take-off and acceleration to climb speed.
50X1 -HUM
SECRET
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 ? CIA RDP8 -0
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FLASELIGHT C
SECRET
TAKE-OFF
DISTANCE
(1000 ft)
January
1957
ALTITUDE
(1000 ft)
60
-
16 17 18 19 20 21 22 23 24 25
40
30
20
10
SL
SPEED
= = 4 MAX POWER
GW 18,600
---- MIL POWER
F-f-'
no,
1111114:774r7
IMMIN: -
Or
- Ng_
.=EGE ffiana
?
500 520
560
600 640
KNOTS
CLIMB
?
ALTITUDE
(1000 it)
60
-MAX POWER
gl: HEACT
T.?=_.-?IC Effelg4
0511101_1 ,
Irma!
ING l
OPERATION AND
egc-41E?OTHERWISE NOTED
CONSIDERED UNLESS.
--ais
18,600LB (CORSI)
16 24
TIME TO CLIMB-MIN
8 12 .16 20 24 28 30'
RATE OF CLIMB
-1 1000 FPM
SECRET
50X1 -HUM
?
SECRET
December
1957
FACEPLATE
?
_Afr
Air __4r?
'411111111,
REMARKS: FACEPLATE is a single place super-sonic wept-wing day interceptor.
-1956
SUMMARY
First observed during the June 1956 Tushino Air Display.
SECRET
50X1 -HUM
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SECRET
FACEPLATE
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
December
1957
DIMENSIONS
Wing
Span 28 ft
Area 230 sq ft
Sweepback leading edge 56 deg
Overall length (w/boom) 50.1 ft
(w/o boom) 42.1 ft
Max depth (fus) 4.4 rt
width 4 ft
Tail
Span 13 ft
Sweep 56 deg
Height from fuselage
center line
7.9 ft
POWER PLANT
No & Model
Type
Length
Diameter
Weight (dry)
Exhaust nozzle
Open
Closed
(1)
Axial flow turbojet
175 inches
38 inches
2950 lb
Diameter
25.6 inches
21.6 inches
WEIGHTS
Loading lb
Empty
Take-off
Combat
Landing, aprx
AR
9,500
13,700
12,400
11,000
6,3.00
ENGINE RATINGS
SL Static
Max
Mil
lb SFC/#/hr/#
12,600 1.85
9,400 0.95
GENERAL INFORMATION
Single place day interceptor.
Tricycle landing gear.
Fixed compression cone in center of intake..
Aircraft may be equipped with a lead pursuit fire control system utilizing IR
and automatic range only radar. If IR is not provided, aircraft will probably
have at least automatic range ohly radar.
Although this aircraft ha z not been observed carrying external fuel it is con-
sidered capable of carrying 2 x 210 US gal tanks.
FUEL
Internal
External
Weight, lb gal
3200 477
2800 420
BOMBS/FREIGHT
Capable of carrying at least the
following:
2 x 2-10 KT 400 lb SPECIAL
OR
2 x 550 lb CLUSTER
OR
2 x 550 lb GENERAL PURPOSE
ELECTRONICS
Radar
Range only radar
IR
IFF SRO type
Navigation
Radio altimeter, low-RV-2
Radio compass - ARK-5
Marker beacon receiver MRP-48P
Communications
VHF RSIU-3M (4 channel)
GUNS
3 x 23 or 30 mm revolver type
120 rds/gun. 6 seconds of fire.
E
ROCKETS
2 x 325 = SCATTERHEAD
OR
2 x 210 mm WE
OR
16 or 38 x55 mm FFAR
OR
Type AAM-1 missiles
OX1-HUM
SECRET
2
1
December
1957
SECRET
FACEPLATE
AIRCRAFT PERFORMANCE
CONDITIONS
Area (to
Intercept
Basic Mission
Area
Intercept
Basic Mission
Area (4)
Intercept
Opt. Mission
Area
Intercept
Opt. Mission
TAKE-OFF WEIGHT (lb)
16,900
6,000
410
74
150
2,100
4,400
14,500
13,700
3,200
410
60
135
1,300
3,000
23,400
16',900
6,000
410
74
150
2,100
4,4400
14,500
13,700
3,200
410
60
135
1,300
3,000
23,400
Fuel at 6.7 lb/gal (lb)
Payload (Ammo) (lb)
Wing loading (Pe)
Stall speed (power off, clean) (kte) '
Take-off ground run at SL (ft) (1)
Take-off to clear 50 ft (ft) (1)
Rate of climb at SL (fm) (2)
Time - SL to 40,000 ft (min) (2)(3)
6.3
3.8
6.3
3.8
Time - SL to 50,000 ft (min) (2)(3)
---
6.3
---
6.3
Service ceiling (100 fpm) (ft) (2)
53,300(1)
52,700
53,300(1)
52,700
COMBAT RANGE (NM)
1,200
---
1,395
595
COMBAT RADIUS (NM)
510 ?
140
610
215
Average speed (kts)
525
535
530
535
Initial cruising altitude (ft)
43,800
51,800
43,800
51,800
Final cruising altitude (ft)
54,000
54,200
54,700
54,700
Total mission time (hr)
2.0
.63
2.4
.92
COMSAT WEIGHT (ib) (5)
13,500(13,500)
12,400
13,200(13,600)
12,200
Combat altitude (ft)
50,000
50,000
50,000
50,000
Combat speed (kts) (1) (5)
700(565)
720
705(565)
725
Combat climb (fro) (1)
5,400
6,400
5,600
6,600
? Combat ceiling (500 fpm) (ft) (1) (5)
59,100(56,600)
61,000
59,600(57,100)
61,300
Service ceiling (100 Ppm) (ft) (1) -
60,000
61,800
68,500
62,100
Max rate of climb at SL (fpm) (1)
47,400
51,000
48,200
51,800
Max speed at SL (kte) (1)
700
700
700
700
Max speed at opt. altitude (kts/ft)(1)
885/35,000
890/35,000
885/35,000
895/35,000
Max mach number at opt. altitude (Mn/ft)(1)
1.54/35,000
1.55/35,000
1.54/35,000
1.56/35,000
,
,
'
NOTES
(1) Maximum power.
50X1 -HUM
(2) Military power.
(3) Includes 0.8 min to take-off and accelerate to climb speed without tanks, or 0.9 min with tanks.
(4) 2 x 210 US external tanks.
(5) Numbers in parenthesis are for aircraft with empty tanks aboard.
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
SECRET
Declassified in Part- Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
1 is
1 !`
SECRET
FACEPLATE
December
1957
TAKE-OFF
DISTANCE
(1000 ft)
-1 r: 1:11 IF-: i I i i E-Iiiil Ft: rti en i.'3".:4-tlitii:
EN SEA LEVEL -.-;-: T., lff E.-.:4 '4- '' :if?
0 !....E B MAX POWER :-.:F. :Its: if.7 -17.1
17^
7:: t ..7",..-: ?!.:'
4II-:
-.:Fri ff. SIKNIFEir !II .:.-..., .4,- ,:-?
?F_ -4' :7.-
Kiff
' hi] c9- tr I
-41.1; F71-
JCLEAR SOFT L-L...;-1,?
:!+!
4+4:
Mg!
14'4!
LT: =!.+5
ffhl: Tr-
rill'''. ;Ht.:
fft
11F
15:11ff
ff: !St GROUND RUN 41;tr,i1qtr,,ttli
Ili' 7- if." Frlf :1" htff F:7174 j.=f
1i ff. ON
211_1'4i i'ttiff ?:141!Ur
12 14 16 18
GROSS WEIGHT (1000 lb)
ALTITUDE
(1000 ft)
60
50
40
30
20
10
SL
SPEED
JI
.!'
MAX POWER
MIL POWER
an lam
mon non
dkr
em rag
Egg
COM ""IIMI int* L
aillmit
BAT WT 12,400'
1
11 11 is ANEEMINIII
111 1111111un '
COMBAT WT 13,900 LB
WI TANKS
t-
ETri
a
500
600 700
800
KNOTS
900
1 I
1000
ALTITUDE
(1000 ft)
70
60
CLIMB
;ATE
MAX POWER,
--MIL POWER,
MEE
resialas45 Eg4 EVE
50 1*1
40
30
WEIGHT REDUCTION DURING
GROUND OPERATION AND E-17.
CLIMB IS CONSIDERED UNLESS
4i-!. OTHERWISE NOTED
ffiff ^ I
20
R/G 12,400 (COMBAT)
CONSTANT
Pat

4
1ff f's C.4 -14.!
;? -LI---
:I ffiTi:
-I
10 _.t: R /G 13,700 LB E'r115'.
1
5 AT T. O. S.- P- TR/C 12,400 LB
V (COMBAT) 1::
CONSTANT hi
SL
O 2 4 6 8 10 12 14 1'6 18 20
TIME TO CLIMB-MIN
22
1 1 1
10 20 30
RATE OF CLIMB
1000 FPM
40
SECRET
50X1-HUM
JanUary
1957
SECRET
FISBBED A
REMARKS: FISEBED A id a single place super-sonic delta-wing day interceptor.
1956
SUMMARY
First observed during the Julie 1956 Tushino Air Display. It is believed to be a prototype.
50X1 -HUM
SECRET
1?
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 ? CIA-RDP81-01043R002000100005 9
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
FISHBED A
DIMENSIONS
Wing
Span 27 ft
Area 265 sq ft
Sveepback leading edge 55.5 deg
Overall length viboom 50.1 ft
(w o boos 42.1 ft
Max depth (fun) 4.4 ft
width 4 ft
Tail
Span 13 ft
Sweep 56 deg
Height from fuselage 7.9 ft
center line
POWER PLANT
No and Model
Type
Length
Diameter
Weight (dry)
Exhaust Nozzle
'pen
Closed
(1)
Axial flow turbojet
175 inches
38 inches
2950 lb
Diameter
25.6 inches
21.6 inches
SECRET
WEIGHTS
Loading
Empty
Take-off
Combat
Landing, &pr.;
ANTE
lb
9,300
13,500
12,200
10,900
6,000
ENGINE RATINGS
SL Static
Max
Mil
lb SFC/#/hr/f
12,600 1.85
9,1400 0.95
GENERAL INFORMATION
Single place day interceptor.
Tricycle landing gear.
Delta wing configuration with swept horizontal and vertical tail.
Fixed compression cone in center of intake.
Aircraft may be equipped with a lead pursuit fire control system utilizing IR
and automatic range only radar. If it is not provided aircraft will probably have
at least automatic range only radar
January
1957
FUEL
Internal
Weight, lb gal
3200 477
BOMBS/FREIGHT
Capable of carrying at least the
following:
2 x 2-10 rr 400 lb SPECIAL
OR
2 x 550 lb CLUSTER
OR
2 x 550 lb GENERAL PURPOSE
ELECTRONICS
Radar
Range only radar
IR
IFF SRO type
Navigation
Radio altimeter, lov-RV-2
Radio compass - ARK-5
Marker beacon receiver )IRP-48P
Ccumunications
VHF RSIU-3M (4 channel)
GUNS
3 x 23 or 30 as revolver type
120 rds/gun. 6 seconds of fire.
50X1-H
..
ROCKETS
2 x 325 as SCATTERHEAD
OR
2 x 210 ma HE '
OR
16 or 38 x 55 as FEAR
OR
Type AAM-1 missiles
UM -
SECRET
7.1)
i
8.
January
1957
SECRET
FISHBED
AIRCRAFT
F) EE R F 0 RM A ts4 (:: EE
'
CONDITIONS
Area
Intercept
Basic Mission
Area
OpIllf::g n
TAKE-OFF WEIGHT
(lb)
13,500
13,500
Fuel at 6.7 lb/gal
(lb)
3,200
3,200
Payload (Amo)
(lb)
410
410
Wing loading
(Psf)
51
51
Stall speed (power off, clean)
(kts)
130
130
Take-off ground run at BL
(ft) (1)
1,200
1,200
Take-off to clear 50 ft
(rt) (1)
2,500
2,500
Rate of climb at SL
(4s1) (2)
20,900
20,900
Time - BL to 40,000 ft
(min) (2)
(3)
4.1
4.1
Time - SL to 50,000 ft
(min) (2)
(3)
7.9
7.9
Service ceiling (100 fpm)
(ft) (1)
58,500
58,500
COMBAT RABGE
(F()
---
580
CCMBAT RADIUS
(NM)
130
195
Average speed
(kts)
535
535
Initial cruising altitude
(it)
49,900
49,900
Final cruising altitude
(ft)
52,600
53,100
Total mission time
(hr)
0.58
0.83
COMBAT WEIGHT
(lb)
12,200
12,000
Combat altitude
(ft)
50,000
50,00(
Combat speed
(kts) (1)
665
670
Combat climb
(fpm) (1)
5,700
6,000
Combat ceiling (500 fpa)
(ft) (1)
59,800
60,100
Service ceiling (100 fpm)
(ft) (1)
60,400
60,700
Max rate of climb at SL
(fpm) (1)
45,800
46,600
Max speed at EJL
(kts) (1)
680
680
Max speed at opt. altitude
(kts/ft)(1)'J.15/.45;,-11
835/35,000
Max mach number at opt. altitude
(Xn/ft)(1)
1 k '35,000
1.145/35,000
NOTES (1) Maximua power.
(2) Military power.
(3) Includes .8 ,in. for take-off and acceleration to climb speed.
am,
SECRET
50X1-HUM
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 ? CIA-RDP81-01043R002000100005-9
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
I1
FISHBED A
SECRET
January
/951
TAKE-OFF
DISTANCE
(1000 ft)
r arillharannranailla
NIIiiIIII
CLEMUrn
M-t;IR1.5.0 FT .
i2IEIIIffnMIIILIIIII NMI
UV laniarms
MOE=
MEIMIRMINIIMIIIME111111
WIIIIIIIIMINIIIMIIIIORU
MIIWIIIIIIIIMMr _L ,
MINiiiiiiillillMar I -r-r :
Effin1111111111Mal GROUND ROLL 1
UsiCAUILUBUIMIINIIUMBIN i
gffilEaliMaillinalIMPOI
MillifOr"_diMENIUMMOKAIRMIRIIII
..addiIIIMIIIIINIM11111111111111.11
amor--...sgamonamas
mmil".`?landgmluilari=
=me mu 1
Illig-I-Blil MI
P.45EZIMME12 A-MINI ?--
10 12 14 16 18
GROSS WEIGHT (1000 lb)
ALTITUDE
(1000 ft)
60
50
40
SPEED
1 I ?
MAX POWER
tio11,L IPOWER
1 ?
I
COMBAT WT 12 206 L...t3
20
10
I 1.
SL 1
500 600 700 800 900 1000
KNOTS
ALTITUDE
(1000 ft)
60
50
40
30
20
CLIMB
I.
1
1
't 17? oc
=---m I
tPOINEk .
' -.17. --1.I., . -- MO_ POWER
4-.. 11?
1_7.; -fr- A - 4= 1' 1 1 1 i
TIC 13,500 LB AT 1.0
---1--,' - 1-:-..-? E,I-- 17 -
:"}:- 74. ,....0-1'... 1 1 1
- 1 1 ...?1 -1
-
el 1 1 I 1
WEIGHT REDUCTION DURING
GROUND OPERATION AND
CLIMB IS CONSIDERED
UNLESS OTHERWISE NOTED
F I
.1_2 _
R/C12',2 00 LB -I?
(COMBAT ) +?
CONSTANT -,-
? 4_ L
4 I
i---- -
' 0
I-11 .
10 :
.1 R/C INITIAL A
i ? R/C I 2200 LB
T COMBAT 1
13.0. WT _
500 LB@ T O. AV / r-.17-T-TfITTJX, 1 )
SL ,
i CONSTANT
I -1
0 2 ? 4. 6 8 10
0
TIME TO CLIMB-MIN
1 I 1 I I I I I 1
IO 20 30. 40 50
RATE OF CLIMB
1000 FPM
SECRET
50X1-HUM
SECRET
January
1957
FISHBED B
REMARKS: FISHaID D is a single-place super-sonic delta-ving day interceptor basically the same
SUMMARY
1956 First observed-during the June -1956 Tushino Air Display. It is beltared to be a prototype.,
50X1-HUM
SECRET
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 CIA
-01 0
SECRET
FISHBED B
Declassified in Part - Sanitized Copy A proved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
January
1957
DIMENSIONS
Wing
Span 25 ft
Area 260 sq ft
Svospback leading ede 55.5 deg
Overall length (v/bo)50.1 ft
(w/o boom 42.1 ft
Max depth (rue) 4.4 ft
width 4 ft
Tail
Span 13 ft
Sweep 59 deg
Height from fuselage
center line 7.9 ft
&ma
POWER PLANT
10 ant Model
T/Im
Length
Diameter
Weight (dry)
Zx'-'it Nozzle
Open
Cloud
(1)
Axial flow turbojet
175 incher
38 inches
2950 lb
Disaster
25.6 inches
21.6 inches
WEIGHTS
Loading
lb
Empty
9,300
Take-off
13,500
Coast
12,200
Landing, aprx
10,900
AWPR
6,000
ENGINE RATINGS
SL Static
lb SICiehri#
12,600 1.85
9,400 0.95
GENERAL INFORMATION
Single place day interceptor.
Tricycle landing gear.
Delta wing configuration with 'wept horizontal and vertical tail.
Fixed compression cone in center of intake.
Fishbed B configuration is the same as FIIUDBED A with the exception of
clipped wing tips and a modified fairing at the horizontal tail-fuselage juncture.
Aircraft may be equipped with a lead pursuit fire control.systet utilizing IR
and automatic* range only radar. If it is not provided aircraft will probably havi
at least automatic range only radar. ,
FUEL
Internal
Weight, lb gal
3200 477
BOMBS/FREIGHT
Capable of carrying at least the
following:
2 x 2-10 KT 400 lb SIMMAL
OR
2 x 550 lb CLUST1R
OR
2 x 550 lb OEM:RAE PURPOSE
ELECTRONICS
Radar
Range only radar
IR
EFF SRO type
Navigation
Radio altimeter, low-RV-2
Radio compass - ARK-5
Marker beacon receivar 2Ep-48p
Communications
VHF RSIU-31 (k channel)
GUNS
3 x 23 or 30 mm revolver type
120 Me/gun. 6 seconds of firs.
,
50
,
ROCKETS
2 x 32 tam OCANTEREZAD
2 x 210 ma Kt
OR
16 or gg x 55 moi FFAR
Type LAM-1 missiles
1-HUM
SECRET
1
07)
Declassified in Part - Sanitized Copy A.provedf Release 2
SECRET
January
1957
FISHBED B
AIRCRAFT PERFORMANCE
CONDITIONS
Area
Intercept
Basic Mission
Area
Intsrcept
Opt. Mission
TAKZ-OFF WRIGHT (lb)
13,500
13,500
Fuel at 6.7 lb/gal (lb) .
3,200
3,200
Payload (Ammo) (lb)
410
410
Wing loading (Psf)
52
52
Stall sped (power off, clean) (kts)
130
130
Take-off ground run at SL (ft) (1)
1,200
1,200
Take-off to clear 50 ft (ft) (1)
- 2,600
2,600
Rate of climb at SL (frm) (2)
20,900
20,900
Time - SL to 40,000 ft (min) (2)(3)
4.1
4.1
Time - SL to 50,000 ft (min) (2)(3)
7.8
7.8
Service ceiling (100 fle) (ft) (1)
58,000
58,000
CCKBAT RAlIGI (101)
---
540
COMBAT RADIUS (NW)
125
185
Average speed (kts)
540
540
Initial cruising altitude (et)
48,700
48,700
Final cruising altitude (ft)
51,400
51,900
Total mission time (hr)
.57
.79
CCKBAT man (lb)
12,200
12,000
Combat altitude (ft)
50,000
50,000
Cat speed (kts) (1)
680
685
Combat climb (fpm) (1)
5,300
5,500
Combat ceiling (500 fpa) (ft) (1)
59,309
59,600
Service ceiling (100 fpm) (ft) (1)
59,900
,
60,200-
Max rate of climb at SL (rpm) (1)
48,300
49,200
Max speed at SD (kts) (1)
680
680
Max speed at opt. altitude (kts/ft)(1)
840/35,009
845/35,090
Max mach number at opt. altitude (Mn/ft)(1)
1.146/35,000
1.46/35,000
..
. ? .
NOTES (1) Maximum pover.
(2) Military power.
(3) Includes .8 min, for-take-off and acceleration to climb speed.
50X1-HUM
. C - 0 3Ron7nnninnnn _
SECRET
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
FIStiEE:
DISTANCE
(1000 ft)
6
-210111.114114L46.Y......mli
SECRET
January
1957
TAKE-OFF
SEA LEVEL
MAX PWR
1-.74,
CLEAR 50 FT 1 _
r I -
ALTITUDE
(1000
(1000 ft)
60
50
40
30
20
SPEED
-COMBAT WI i2,2-00 LB
L
MAX POWER!
MIL POWER I
?
: 1
-1
,? l-:
GROUND RUN1 .
- .,.. - ' 1:- .1 .1"
-. :" 77H-1-11\T .
10
!., :1 -t
-4--
SL --
8 10 12 14 16 18 500
GROSS WEIGHT (1000 lb)
600
700
800
KNOTS
900
1000
ALTITUDE
(1000 ft)
60
.CLIMB
1f4T-Tt?iiIiaii
?wit=
50
40
30
20
T/C 13,500LB AT T.O.
M:EgERE
A- MIMEO
MAX POWER
--MIL POWER
?
EgirAisi
EMMEMEE
'EFT-
Jj R/C 12,200 L B (CuM BAT) `-'1?.t_tF-
E CONSTANT
i1.1r7
11.
WEIGHT REDUCTION DURING
GROUND OPERATION AND
"IL4 CLIMB IS CONSIDERED UNLESS
Ell OTHERWISE NOTED
10
p TO. WT
17 13,500 LB '
,AT T.O.
1.4 4
_ -
SL
1 I
0 2 4 6 8
TIME TO CLIMB-MIN
I 1 I 1 I 1 I ( 1
10 20 30 40 50
RATE OF 'CLIMB
000 FPM
tar-T,
7111
-.11r7;r'
R/C 121200L8
(COMBAT)
CONSTANT
?
10
411.16.11.11.1.?.611.anlif
????????1
Cr
SECRET
50X1-HUM
^
SECRET
January FISHPOT
1957
REMARKS: FISHPOT is a single-place supersonic delta-wing limited all-weather interceptor.
SUMMARY
1956 First observed during the June 1956 TUshinoAlr Display. It is believed to be an experimental
prototype. Aircraft may be developed for future operation.
50X1-HUM
SECRET
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
7
SECRET
FISHPOT
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
January
1957
DIMENSIONS
Wing
Span 24 ft
Area 250 sq ft
Sveepback leading edge 58.5 deg
Overall length (v/boom) 50.25 ft
(w/o boom) 42.65 ft
Diameter 4.16 ft
Tail
Span 12.75 ft
Sweep 58 deg
Height from fuselage
center line 7.7 ft
POWER PLANT
No & Model
Type
Length
Diameter
Weight (dry)
Exhaust Nozzle
Open
Closed
(1)
Axial flow turbojet
188 inches
42.25 inches
3500 lbs
Diameter
28.1 inches
23.6 inches
WEIGHTS
Loading
Empty
Take-off
Combat
Landing, aprx
AMIE
lb
9,900
14,900
13,600
12,000
6,100
ENGINE RATINGS
St Static
Max
Mu
lb SPC/#/hr/#
15,200 1.90
11,200 0.95
GENERAL INFORMATION
Single place limited all weather interceptor.
Tricycle landing gear.
Slightly clipped delta wing configuration with swept horizontal and vertical
tail.
Fixed compression coni above air intake may house AI gear capable of short
range search track.
FUEL
Weight, lb gal
Internal 3700 552
BOMBS/FREIGHT
ELECTRONICS
Radar
Search track Al
IFF SRO type
Navigation
Radio compass AR1C-5
Radio altimeter, Low-RV-2
Marker beacon receiver m2F-48p
Ccamomications
VHF RSIU-3M (8-12 channel)
GUNS'
No armament apparent on aircraft
sighted. Developed, aircraft may have
1 x 37/30 mm Gatling 120 rds 5(
(1-2 sec)
ROCKETS
38 x 55 mm FFAR in 2 external pods
(1 under each wing) '
OR 2 x 220 mm Discreet frag.
OR.2 x 220 mm with 10'.' 2-10 kt
nuclear heads
OR. Type AAM 1, 2 missiles
Xl-HUM
SECRET
SECRET
January
FISHPOT
AIRCRAFT PERFORMANCE
CONDITIONS
jBasic
Area
Intercept
Mission
Area
Intercept
Opt, Mission
TAKE-OFF WEIGHT
(lb)
14,900
14,900
Fuel at 6.7 lb/gal
(lb)
3,700
3,700
Payload (Ammo)
(lb)
410
410
Wing Loading
(psi)
6o
6o
Stall speed (power off, clean)
(kta)
140
140
Take-off ground run at SI
(ft)
1,200
1,200
Take-off to clear 50 ft
(ft)
2,400
2,400
Rate of climb at SL
(fpm) (2)
27,400
27,400
Time - SI to 40,000 ft
(min) (2)(3)(4)
3.4
3.4
Time - St to 50,000 ft
(min) (2)(3)(k)
6.7
6.7
Service ceiling (100 fpm)
(ft) (2)
50,700
50,700
COMBAT RANGE
(m)
420
555
COMBAT RADIUS
(n)
65
.
130
Average speed
(kts)
540
540
Initial cruising altitude
(ft)
50,700
50,700
Final cruising altitude
(ft)
53,100
53,800
Total mission time
(hr) (3)
.34
.58
COMBAT WEIGHT
(lb)
13,600
13,400
Combat altitude
(ft)
50,000
50,000
Combat speed
' (kts) (1)
980
980
Combat climb .
(fga) (1)
6,300
6,500
Combat ceiling (500 fla)
(ft) (1)
59,000
59,300
Service ceiling (100 fpm)
(ft) (2)
52,500
-
52,900
Max rate of climb at SL
(4m) (1)
57,200
58,000 .
Max speed at SL
(kts) (1)
800
800
Max speed at opt. altitude
(kta/ft)
1090/35,000
1090/35,000
Max mach number at opt. altitude
(Mn/ft)
1.90/35,000
I60/35,000
,
.
'
NC)TE S (1) Maximum power.
/
2) Military power.
3) .7 minutes to accelerate to V climb included.
(4) Allows for weight reduction during ground operation and climb.
50X1 -HUM
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
SECRET
Declassified in Part- Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
MAX POWER
--- MIL POWER
!IT gip T,41.,113ampapr!li
dUi GW 13,600
ettr.9r. ? g ?r
illAtrii!Cki MI!
tli;t1ti
-r;
I afilfii
FilE
. ?ii-ngi
:tiann = ?
:111
Fri
It:. Mita:
:.'#111171.1
AAX POWER
ig :=4"; iii! qi? ? --- MIL POWER
----1- r e glIVIRIXE IC 14,900LB AT T.0..'"
liv-?;;;''' 'i-: N ini iffi iiii
Ilkjii i-- . INt., IR'
-,?,-,": Otrii; Rfiliiiii5K4.1iiiii;
WEIGHT REDUCTION DURING
GROUND OPERATION AND 1
CLIMB CONSIDERED UNLESS 1
, OTHERWISE NOTED
REMARKS
? ? FIIXEH is a single-place supersonic swept-wing day interceptor.
First observed during the June 1956 Tushino Air Display.
in operation in the near future.
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
F:
41
SECRET
FITTai
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
December
1957
DIMENSIONS
Wing
Span 26.5 ft
Area 250 eq ft
Sweepback leading edge 62 deg
Overall length (w/boom) 46.3 ft
(w/o boom) 41 ft
Diameter 4.16 ft
Tail
Span 12.75 ft
Sweep 55 deg
Height from fuselage
center line 7.7 ft
POWER PLANT
No & Nadel
Type
Length
Diameter
Weight (dry)
Exhaust Nozzle
Open
Closed
(1)
Axial flow turbojet
188 inches
42.25 inches
3500 lbs
Diameter
28.1 inches
23.6 inches
WEIGHTS
Loading
Empty
Take-off
Combat
Landing, sprx
APR
lb
10,300
15,300
14,000
12,300
6,800
ENGINE RATINGS
SL Static
Max
Mil
lb EFC/#/hr/#
15,200 1.90
11,200 0.95
GENERAL INFORMATION
Single place day interceptor.
Tricycle landing gear.
Intake provided with translating compression cone.
Aircraft may be equipped with a lead pursuit fire control system utilizing
IR and automatic range only radar. If it is not provided, aircraft will
probably have at least automatic range only radar.
Although this aircraft has not been observed carrying external fuel it is con-
sidered capable of carrying 2 x 210 US gal external tanks.
FUEL
Internal
External
Weight, lb gal
3700 552
2800 420
BOMBS/FREIGHT
2 x 2-10 KT 400 lb SPECIAL
OR
2 x 250 lb CLUSTER
OR
2 x 250 lb GENERAL PURPOSE
ELECTRONICS
Radar
Range only radar
IR
IFF SRO type
Navigation
Radio altimeter, low-RV-2
Radio compass ARK-5
Marker beacon receiver 191P-48P
Communications
VHF RSIU-3M (4 channel)
GUNS
No armament apparent on aircraft
sighted. Developed aircraft may have
3 x 30 or 37 an revolver type,
100 rds/gun. 5 seconds of fire.
ROCKETS
2 x 325o SCATTERBEAD
B x 210 an HE
QR
16 or 30 x 55 an FFAR
OR
2 x 220 an Discreet frag
OR
Type AAM-1 missiles
11.1.1>i
50X1 -HUM
SECRET
1
SECRET
December
1957
FITTER
AIRCRAFT PERFORMANCE
CONDITIONS
Area (6)
Intercept
Basic Mission
Area
Intercept
Basic Mission
Area (6)
Intercept
Opt. Mission
Area
Intercept
Opt. Mission
TAKE-OFF WEIGHT (lb)
18,500
6,500
410
74
15,300
3,700
410
61
18,500
6,00
410
?
74
15,300
3,700
410
61
Fuel at 6.7 lb/gal (lb)
Payload (Ammo) (lb)
,Wing loading (Per)
Stall speed (power off, clean) (kts)
150
135
150
135
Take-off ground run at SL (rt) (1)
1,700
1,100
1,700
1,100
Take-off to clear 50 ft (ft) (1)
3,200
2,300
3,200
2,300
Rate of climb at SL (fpm) (2)
15,100
27,100
15,100
27,100
Time - SL to 40,000 ft (min) (2)(3)(4)
5.6
3.5
5.6
3.5
Time - SL to 50,000 ft (min) (2)(3)(4)
---
6.4
---
6.4
Service ceiling (100 fpm) (ft) (2)
46,100
52,000
46,loo
52,000
CCERAT RANGE OW
1,065
455
1,245
590
COMBAT RADIUS (NM)
390
75
48o
140
Average speed (kts)
525
535
530
535
Initial cruising altitude (ft)
45,400
51,700
45,400
51,700
Final cruising altitude (ft)
53,900
54,100
54,700
54,700
Total mission time (hr) (3)
1.6
.37
1.9
.60
COMBAT WEIGHT (lb) (5)
15,200(15,600)
14,000
14,900(15,200)
13,800
Combat altitude (ft)
50,000
50,000
50,000
50,000
Combat speed (kts) (1) (5)
1,000(880)
1,035
1,000(895)
1,035
Combat climb (fpm) (1)
5,400
6,400
5, 600 -
6,600
Combat ceiling (500 fpm) (ft) (1) (5)
58,300(58,800)
60,000 ,
58,80056,800)
60,400
Service ceiling (100 fpm) (ft) (2)
"52,200
53;900
52,700
54,200
Max rate of climb at SL (fpm) (1)
54,200.
59,000
55,400
60,200
Max speed at SL (kts) (1)
800
800
Boo
800
Max speed at opt altitude (kts/ft)(1)
1,180/35,000
1185/35,000
1,180/35,000
1185/35,000
Max mach number at opt. altitude (Mn/ft)(1)
2.05/35,000
2.06/35,000
2.05/35,000
2.06/35,000
NO TE' (l) Maximum power.
(2) Military power.
(3) .7 minute to accelerate to V climb included.
(4) Allows for weight reduction during Ground Operation and Climb.
(5) Numbers in parenthesis are for aircraft with empty tanks aboard.
(6) 2 x 210 US gal external tanks.
50X1 -HUM
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
. SECRET
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
--
SECRET
Dece:tbei
1957
CONFIDENTIAL
1 U. S. S. x.
TAKE-OFF
SPEED
DISTANCE
(1000 ft)
ALTITUDE
(1000(t)
MAX POWER
--MIL POWER
GROUND F.UN
I
? 71?
T. .L. 1-1
-4 1- 1
0 600 800 000
1200 1400
COMBAT WI 5,600 LB
W/TANKS
Ti
GROSS WEIGHT (1000 lb)
CLIMB
ALTITUDE
(1000 It)
a.
60
? MAX POWER
MON MMI --- MIL POWER.
INE111111111111111
1
T/C 15,300 LB AT T 0.
j I
I
? WE GHT REDUCTION DUR NG
GROUND OPERATION AND
? :'CLIMB CONSIDERED UNLESS
'OTHERWISE NOTED
4?-1-1.
14,000 LB (CONST).
14,000 LB
(CONST.)
I
15 300 LB s.?
NA
AT T.O. r?
,
10. 20 30 40 50
RATE OF CLIMB-1000 FPM
[11111 ?I I
2 3 4 5 6 7 8 9
TIME TO CLIMB -MIN
50X1 -HUM
I DESCRIPTION I
Low-wing monoplane. The center section of the wing, which is probably integral with
fuselage main section, has a slightly swept-back leading edge. The trailing edge sweeps
forward from root filleto. The fuselage is reported to be shorter, slimmer and lighte-
. than that of the 11-2. In 'general, characteristics are probably very similar. 50X1 -HUM
SECRET
CONFIDENTIAL
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Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
CONFIDENTIAL
n
11-10
Mfr.
Demlinar: Ilyuabin
Type Attack Bailer (Ground Attack)
Crew
2
PERFORMANCE
July
195.3
Maximum Speeds: 262 knots e S.L.; 273
Cruising Speeds: Normal Power______ knots
Climb: 5.0 mins. to 10000 ft A
Service Ceilings.: ft with
Take-Off distance over 50 ft obstacle
knots g 5500 ft alt.; 222 knots g 20000 ft alt.
e ft alt.; Economical knots g ft alt.
It.; Rate of Climb:_ 1950 ft/min. at SL ft alt.
normal weight; 23500 ft with 13090 . lbs weight
Concrete 2400 Turf 2500 ft into zero wind at Sea Leval
Fuel: (US gals.) internal; Normal191___
nautical Wes
o2Ailknots,_50(X_L_ft alt.
with igUS gals. of fuel
and lbs beam
Combat Radius: 170 Nautical Niles
Maximum ; External: Normal , maximum
RANGES
nautical miles
I knots, ft alt.
with US gals, of fvel
.and lbs
POWER PLANT
nautical miles
? knots, ft alt.
with US gals, of fuel
and lbs
No. Engines 1 Take-Off 1975 hp- 4 SL ft alt. 2500 rpm 61ln. Hg.
1730 _hp. .17.:3553ft alt. 2350 rpm 52.5 in. HI-
Type Engines Racit.rdoatillt Military he. e ft alt.
War Emergency he. 4 ft alt.
A3l-42, 12-cylinder, upright "V", liquid-cooled
Normal
Description
rpm in. Mg.
rpm in. Hg.
SPECIFICATIONS
Gore 6.24 ins
StrobelemMAns
DIspl.___2_
2 0 ss. Ins
Comp.Ratioad:a.
SUPERCHARGER
PROPELLER FUEL
Dry Wt. 2260 No. Speeds_1 Mfr. ANL-5L-24 Type95/115.95/130
Gasoline
Red.O?er .6:1 No. Stages _1 No.illades 3
Eng.Width__IL.ILJAIRatios 11'1 Dia. 11 ft,10 ins
Eng.Langth_94_1311mpoller DiaiLL4Lins Pitch Control Nrdraulic
ARMAMENT
BOMB/FREIGHT LOAD
COMSAT PROTECTION
Guns
232331. in ring NrYA
2x7.62 in wing SNICAS
1:12.7 mei 1i:ix:over turret in
rear end of cockpit. BEREZINA
Rockets: 2x132 mm under wing
Gunsight -la ref stator Ube
Normal Load 880
Maximue Load 1320
Stowage:
lbs
lbs
6x220 ib bombs or
8Xl10 lb bombs
Istbsight Unknown
?
SPECIFItATIONS
Armor Juliet proofirimmlableld.
7Uselage from rear of cockpit
. forward is sheathed in 6.5 me
41111ar.
Armor behind gunner.
Fuel Tanks Protected
Materials
lellgth:__35._ft,Ja_in; Height: ft,
Haight.: Airframe lbs; Normal Gross -W546 lbs; Maximum Gross 14980
All metal construct . ?
In; Gross Wing Area 123
sq. ft
lbs
ADDITIONAL DATA
The I1-10 is a development of the 11-2 with Mart1:VeLtIni.i. engines. It became operational in
1944 and is replacing the 11-2 "Stamina". It is cwregmly in production and is in use in large
maws in the Soviet Air Force as a round attack aircraft. It has the same armor covering as the
11-2, 6.5 mu plating over the engine and cockpit and behind the gunner's seat. The bomb installation
is belitVeni to 'consist of two internal bcab-baya in the ring roots and external racks under the fuse-
lage. LO14 radio equipment is fitted.
Performance data shown are used at latest available USAF flight test data (Nay 1952).
CONFIDENTIAL
?
?
50X1-HUM
41
?
?
?
CONFIDENTIAL _
July
U.,sP
1953
ALTITUDE - FEET
25000
Z0000
15000
,10000
5000
S. L.
11-10
11111111:1111111
la O
1 11M..1111.I
1111111111111111111111111
1111111111111111111 6.1111111111111:111111111111:11
11111111111111!11111:11:::1111:11811:191111111111111111111111111111
11111:1:1:1:ffii iiiia.iiima
iiilli111111110111111111111
111111111111111P?"11111411111iiiiiiillill1111111111111111111111
111111111111111111111111111111111111111111111111111111111111 111111111
1111111111111111111111111111111
1111111111111111111111111101111111111111111111111111111111111111111
Max. S eed
MEMMIIMMLUL! alpsimitilmompommoll
mmuommotrimmimormahmhindummmi
1111111111111110111011111111111111111111111111111111111111111 II
lllidorpommummollopmmummumiimi
MINN
Rate of Climb !
Ink Time to clitooti 1111111111111111111111PAI 11111111111
r"H111111-111 PPR ill
R/C - 1000 FT/MIN o
0.5 1.0
1.5 2.0
2.5 3.0
SPEED ? KNOTS
MIN TO CLIMB
tOo 3.00 ' 400 500 660
4 8
16
24
Pe OrMa. e
DESCRIPTION
(1) Take-off Power (2500 RPM)
Gross Weight 13020 lb
(2) Normal Rated Power (2350 RPM)
Gross Weight 13090 lb
50X1-HUM
Performance curves based on USAF flight test. Take-off Power limitation precludes its
use for climb.
CONFIDENTIAL
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I PERFORMANCE
I n s
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CONFIDENTIAL
11-10
U.S.S.R.
Stay
3750
t:
.2(5L__:)0
0
a 3230
..3.0C.20
ILI 2750
48
11)
w 2250
a
1750
INga
TAKE-OFF
I '
I
- Concrete rummy
-- -- Turf rummy
1
1[1 I
11,;-11 I
NS 11111 M.111111111111.
nivaiwai 111111Ill

11111111111111111111
w.
1511111111RMINNIIIIIIIIMWSIIIRMIIIIIMIN 7?
? IMININIIIMINISMIBMIMINIMIll
011111111111115111111111
11111MIVIRI111111
5111?1151?1151a1MIMIIIMMINM1551?115 II
itiminamoomminiumuna mainiiiirAmila
111111111
5I1 IIIIMMINIMINNINIIMIWIN NW MAIM.
111111111111111111 ,adigiligi
IIIII
pion= .dAi orn
.4_
maw EArluz.i. en
II 1111
1
i
i
SRO' WT.-1000 L5S 12.0
fl
1
1
un-
13.0
14.0
15.0
1.6.o
17'.0 18.0
1953
DESCRIPTION
CONFIDENTIAL
? ID
50X1 -HUM
? ?
CONFIDENTIAL
March
1952
Tu-2
Tu-2
DESCRIPTION
It is a twin-engine, shoulder-wing monoplane. Engines are underslung in long slender
nacelles. The air scoop is prominent on top of the engines. A large diameter propeller
spinner is fitted. The fuselage has deep oval shape and appears quite slender with sharply.
pointed nose. Lower half of the nose is pleriglass-covered. There is pronounced dihedral
in horizontal tail and oval-shaped twin-rudders are fitted. .A gunner's position is on50X1 -HUM
top of fuselage behind wing, also ventral gun position with several observation window.
is provided.
CONFIDENTIAL
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CONFIDENTIAL-
Tu-2
Tu-2
Mfr flasiErer. Pflpninv
Type Light Bomber
Crew
1 mr
PERFORHANCE
March
1952
Maximum Speeds: 250 knots d S.L.: 278 knots 1 15500 ft alt.; 250 knots w 25000 ft alt.
cruising Speeds; Normal Power 250 knots 0 15000 ft alt.; Economical 180 knots i 20000 ft alt.
Climb: 6.2 mins. to 10000 ft alt.; Rate of Climb: ? 1730 ft/min. at SI, ft alt.
Service Ceilings: 29000 ft with normAl_lilJght: ft with lbs weight
Take-Off distance over 50 ft obstacle 2000 ft Into zero wind at Sea Level
Fuel: (US gals.) Internal: Normal 715 , Maximum 875 : External; Normal , Maximum
COMBAT RANGES
850
nautical
miles
ft alt.
1010 nautical
ft
of
miles
alt.
fuel
125
nautical
miles
alt.
fuel
IP, 178 knots,
10000
?_178 knots, 10000
a 178 knots,
10000 ft
with 715
US gals.
bombs
of fuel
with 875 US gals.
with 125
US gals, of
bombs
and 1100 lbs
and 2200 lbs bombs
and 7000 lbs
Combat Radius: 400 Nautical Miles Combat Radius: 500 Nautical Miles Combat Radius: 50 Nautical Miles
POWER PLANT
No. Engines 2 Take-Off 1825 hp. e SL
16750 ft alt 2500 rpm 48 in. Ng.
Normal
11A hh:. ?: ft alt 2400 rpm in. Hg.
Type Engines Reciprocating military rpm 40.1 In. lig.
War Emergency hp. e ft alt. 2400
ft alt. rpm in. Hg.
5400
Description ASH-82 FNV, 14 cylinder, air-cooled radial
SPECIFICATIONS
SUPERCHARGER
PROPELLER FUEL
Bore 6.1 ins Dry Wt. 1980 No. Speeds 2 nfr. AV-5 Type. Gasoline
Stroke 61 Ins Red.Gear 1.45:1 No. Stages 1 No. Blades 3 5.)/I15.95/130.
Displ. 2555 Cu. Ins Eng.Width 49.5 in. Ratios 7.14 & 10:1 Dla. 13 ft, 0 ins
Eng.Length 79 in,, Impeller. Die _Ins Pitch Control Constant speed nonfeathering
ARMAMENT
BOMB/FREIGHT LOAD
COMBAT PROTECTION
Guns
Normal Load 3300 lbs
Armor ?
2x2Omm/15Orpg. Fixed, wing rootsMaximum
Load 7000 lbs
9mm. armor behind pilot.
lx12.7mm/150rPe. Flex. rear
Stowage: Internal.
Pilot and gunners protected.
cockpit.
9 x 220 lb.' bombs, or
lx12.7mm/25Orpg. Flex. Upper.
3 x 1100 lb. bombs, or
1x12:7mm/350rog. Flex. Lower.
15 x 220 lb. bombs
Stowage: External. 2 torpedoes ur
2 x 2200 lb. bombs
Gunsight Pilot: PBP-la,
Boibsight OPB-ID
Fuel- Tanks Self sealing.
Upper- PEIP-1, Lower: OP-2L
SPECIFICATIONS
Materials All metal construction
Span:_61_ft,___In; Length:_45._ft,2_in; Height' 15 ft,_:1,11_1n; Gross Wing Area 510 sq.ft
Weights: Airframe 8600 lbs;? Normal Gross 24460 -lbs; 'Maximum Gross lbs
ADDITIONAL DATA
One of the U.S.S.R.'s latest operational bombers. /First placed in operational use in 1944 and
is still their main first line light bomber. The ASH-82 FNV engine is improved model of the U.S.
Wright R-2600 engine built under license. I.F.F., high frequency transmitter-receiver, interphone
amplifier, and an RPKO-10M radio compass are installed.
CHARACTERISTICS OF FO FIGN AIRCRAFT
CONFIDENTIAL
50X1-HUM
4111
?
CONFIDENTIAL
March
U.S.S.R.
Tu-2
1952
SPEED 8 C1/MB
40000
35000
30000
25000,
1:20000
a
4
UM!.
10000
140._
2500
S.L.
R/0 "MOO FT/NIN0
I
1
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.
1
In
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300
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10 20 30 40 50 60
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PERFORMANCE
DESCRIPTION
(:) MILITARY Pasn, NORMAL GROSS WT. 24255 LBS.
50X1-HUM
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
CONFIDENTIAL
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
CONFIDENTIAL
Tu-2
U.S.S.R.
March
4
0
0
0
4
F
4
011065 WT
TAKE?OFF
3500
+H+1-rr9
I
---F'
4 1,
1-14
1 ' : ;
-i-i-H-
-i-/-1-',.
' ! ' 14--4--1-1-14-
1--7--
-7-#P
11-
3250
ti_i:=Ltr
: : 1 :
--z----a,iiiii :- rim;,.-y-i
----Turf runway
-F-1-
_r___-ri-
--;-4-
-I i 1 ;
-H-FF
-H-H-
'-i-.-2 '
?_ri-ii:-,-
,
-Fri--
I 1 . L-1-r_r
---.T-1-
. I I;
, ; f.
. ? , .
, , ,
3000
'
-;-?-?-
-7-_
-4- --
. , ,

i-r-r
-r-rrt
4.-:,---T_
,
_, ri-
7.-r-
; 111;7;:
-'-1-7-'
.+1_,_
-k-IH-;1,;
_i__t_j__L
I.i'l
_
;;II
11'.?
--i-4-H-
,.4
' v-"--'
-
2750
I I
--1-4-I-
,
-1-L-i-r
I I I .
: I, */-,
,-,-.
i1 ' '
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. , ,
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-ri-n-
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; I ?
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+
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1
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i
4
-: i-T-
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+7-17-
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:
2500
'.--d--H1-1-
-1.+P-
--+
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4-r1-1--1-1-?
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f-
-f t 1-1
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-F-
!''!
,if t
2250
-4-i-H-11
'
+41-4-
/I,
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1 ,I1
r-/ ;
, ,t -
,
"r,---I-;
1 ' ,
, i-H-
: :
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-4. !
-L-t--17-
1 III
-H-i-I,
-',--f- '
I ?
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1
I
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-1-r;?
H-
Jr--
'
%1-
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-H4 .-i-
;
, :
2000
H ,
-14-i-4-44-'
. '
i-
EH'
-1:
?H---1---1--
-r I--r
-)-}-f-4-
h_,_
-T2
' , 7
,
'
'
,

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i I ,
- ..1-I?k
.
-r-i-,,,',-
,i;
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;
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. LL
_L_
.
I
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?,
,
,
1500
-!`"
i
-Hu-

-rri-t
r; 1-',-
?
;
am ,

,,
,
no LBs
30
32
34
1952
PERFORMANCE
DESCRIPTION
CONFIDENTIAL
50X1-HUM
?
?
?
January
1958
CONFIDENTIAL
BULL
REMARKS: BULL is a mid-wing four-engined monoplane. Engine nacelles extend well forward of the
leading edge of the wing. The inboard nacelles extend beyond the trailing edge of the wing. Wings
taper to square tips. Fuselage is circular with the nose extending well forward of the engines. Single
tail with prominent fin. Tricycle landing gear with dual wheels is fully retractable.
SUMMARY
BULL is a copy of the U.S. B-29A acquired by the Soviets in World War II. The USSR credits the
aircraft to the designer TUPOLEV. The Soviet designation is TU-4. BULL has been operational in the
USSR since 1948: but has been largely replaced by more modern jet aircraft.
50X1-HUM
CONFIDENTIAL
1
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Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
Z.,
CONFIDENTIAL
TU-4
Tu-4
Mfr Designer: Tnrolav
Type Bomber
Crew 11
PERFORMANCE
March
1952
Maximum Speeds. 262 knots a S.L.; 350 knots 00000 ft alt.; 132 knots 6 25000 ft alt.
Cruising Speeds: Normal Power 302 knots t 25000 ft alt.; Economical 19R knots t innnn ft alt.
Climb: 32.0 mins. to 35000 ft alt.; Rate of Climb. 1620 ft/min. at SL ft alt.
Service Ceilings: 39550 ft with normal weight; ft with lbs weight
Take-Off distance over 50 ft obstacle 7825 ft Into zero wind at Sea Level
Fuel: (US gals.) Internal: Normal 7748 , Maximum ; External; Normal . Maximum
RANGES
3100
nautical
miles
2140
nautical
miles
1660
nautical
miles
s 175
knots,
10000
ft
alt.
t 179
knots,
10000
ft
alt.
e 167
knots,
10000 ft
alt.
with
7748
US gals.
of
fuel
with
6080
US gals.
of
fuel
with
4415
US gals, of
fuel
10000
lbs
and 20000
lbs
and
10000
lbs
and
Bombs
Bombs
-
Bombs
Combat Radius: 1700
Combat Radius: 1230
POWER PLANT
Combat Radius: 880
Engines 4 Take-0ff?2200
hp.
a ST,
ft
alt
2800
rpm
in.
Hg.
Hg.
Hg.
Hg.
No.
2000
hp
t 25000
ft
alt.
2400
rpm
in.
Normal
Type Engines Reciprocating military 2200
hp.
la 250100
ft
alt
2600
rpm
In.
War Emergency
hp.
a
ft
alt.
rpm
In.
Description
..ASB 90, l8 rylirviar, air?eool.d radial
(Believed to be a copy of the U.S. Wriz)it R-1350)
SPECIFICATIONS
SUPERCHARGER
Bore 6.125 ins Dry Wt. 266R No. Speeds Turbo Mfr.
Stroke___LL_Ins Led.Gear 2 861 No. Stages No.Blades 4 100-130 grade
Dispi. cu. ins Eng.Width 56 in. Ratios 6.01 Dia. 16 ft, 6 ins
Comp.R;TI;8088: 1 Eng.Length 76 In. impeller Diaal__Ins Pitch Control Hydromatio
PROPELLER FUEL
Type Gasoline
ARMAMENT
BOMB/FREIGHT LOAD
COMBAT PROTECTION
Guns 2y12 7 alpper 'turrets
Normal Load 10000 lbs
Armor Unknoun
2.02 7mm Lever TnrunrA turret
maximum Load 20000 lbs
--2x12-7=?Lawer?roar-4ur-rat.--
3x12.7mm tail turret
Bomb loads probably similar
Howevor, 2101mm inetellntinne
to U.S. B-29
have been lean in turrets_
,
Guns ight MaV be copy of U.S.
BoabsightPnaaibly nermen
Fuel Tanks Unknown
eentrel fire enntrml eyetem
Latfe 7 type
SPECIFICATIONS
50X1 ?HUM
atUf
12
All metal oonatruction
Materials sq. ft
99 fte_p_in: Height:-27_ft,_101Lin; Gross_Wing Area 1736
Span42:_fte_l_in; Length:
Weights: Airframe 48000 lbs; Normal Gross 1L0,000 lbs; Maximum Gross 140,000 lbs
ADDITIONAL DATA
This medium bomber is a
main differences are the substitution
changes which are not aPparent
Tupolev, and it is their standard
except for the tail-turret and
and the radius to 2150 NM in
the B-29A.
copy of the US B-29A aircraft acquired by the Soviets in WW II. The
of Soviet guns for the US guns, and the possibility of internal
from photographs. The USSR credits the aircraft to the designer
medium bomber today. While the removal of the defensive armament
the addition of the fuel would increase the combat range to 3960 NM
the stripped version. the above figures are based on US performance for
CHARACTERISTICS OF F 4AFT
March
1952
CONFIDENTIAL
Tu-4
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()MILITARY PGNER, COMBAT GROSS WT. 101470 LBS.
CONFIDENTIAL
50X1 ?HUM
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Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
Tu-4
TAKE-OFF DISTANCE OVER 50 FT. OBSTACLE. ,-FT.
10000
9000
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7000
6000
5000
4000
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1 PERFORMANCE 1
DESCRIPTION
CONFIDENTIAL
50X1 -HUM
fre
?
Jan
CONFIDENTIAL
31:-1
Type-31
1954
AnIQ Fr*s 0-498A
7 1114 BO
AAAAA Ct1 4100.1 101W 04A. 14 OCT 44.
1141C14 MBY St OHO.
Type -31
DESCRIPT1O.N
This horrybouber was first seen at the July 1951 air @how at the TUshino Airfield
in Moscow.
CONFIDENTIAL
50X1 -HUM
1 1
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
CONFIDENTIAL
CONFIDENTIAL
BEAGLE (IL-28)
Mfr Designer Tupolev Crew
Type Heavy Boiber
PERFORMANCE
Maximum Speeds; knots e S L ; knots 0 ft alt.; of:nots a ft alt.
Cruising Speeds: Normal Power knots e ft alt.; Economical knots e ft alt.
Climb' sins, to ft alt.; Rate of Climb: ft/min. at ft alt.
Service Ceilings: ft with normal weight; ft with lbs weight
Take-Off distance over 50 ft obstacle ft into zero wind at Sea Level
Fuel: (US gals.) Internal: Normal 9975 , Maximum ; External: Normal , Maximum
RANGES j
nautical miles
? knots, ft alt.
with US gals. of fuel
and lbs
3700 nautical miles
? 185 knots, 25000 ft alt.
with 9975 US gals, of fuel
and 0 lbs Bombe
Radius: 1850 NM
nautical miles
? knots, ft alt.
with US gals. of fuel
and lbs
POWER PLANT
No. Engines 4 Take-Off 2700 hp. 0 HT, ft sit rpm In. Ng.
Normal 2500 hp. p 25,000 ft alt. rpm in. 111g.
Type Engines Reciprocating military hp e ft alt. rpm In. lig.
War Emergency hp. e ft alt. rpm in. Hg.
Description Assumed improved version Soviet ASH-90
SPECIFICATIONS SUPERCHARGER
PROPELLER FUEL
Bore ins Dry Wt. No. Speeds Mfr Type Gasoline
Stroke ins Red.Gemr No. Stages No?Blades 4 100/130 grade
Displ. cu.ins Eng.Width Ratios gis, 17 ft, ins
Colo. Ratio Eng. Length impeller Dia_____Ins Pitch Control
ARMAMENT
BOMB/FREIGHT LOAD
COMBAT PROTECTION
Guns
Normal Load
lbs
Armor
Maximum Load
lbs
..
Gunslght
Bodbsight
Fuel
Tanks
SPECIFICATIONS
Materials
Length:_lacLft,___In: Height. ft, In; Gross Ming Area 287n sq.ft
Weights: Airframe lbs; Normal Gross 160,000 lbs: Maximum Gross lbs
ADDITIONAL DATA
The exact engines installed are unknown; however, the 1951 Type-31 characteristics,and performance
are estimated for improved Soviet ASH-90 engines assumed to be available immediately prior to July 1951.
On the basis of the estimated power plants installed, the aircraft appears to be a prototype, pending
installation of more powerful engines.
For reasonable operational performance, it is estimated that engines of approximately 5000 SHP, BHP
or equivalent thrust will be required. To give on indication of the aircraft's capabilities with ade-
quate power, performance is shown below for an assumed installation of is x Ju mo 022 turbo prop engines.
Take-off Weight -- 210,000 lb.
Bomb Load -- 10,000 lb.
Max Speed (at 35,000 ft.) -- 325 kts.
Rate of climb -- 2,000 fpm at S.L.
Combat Ceiling -- 35,000 ft.
Range/Radius
50X1-HUM
REMARKS: The IL-28 (BEAGLE) is a twin-jet light bomber designed by IMUSHIM. It has a straight
SUMMARY
1955 First appeared in operational numbers in the May Day 1950 Airshow in Moscow.
operational use in the Soviet and Satellite Air Forces.
Airc50X1-HUM
CONFIDENTIAL
CHARACTERISTICS OF FOREIGN AIRCRAFT
CONFIDENTIAL
Declassified
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Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
5
CONFIDENTIAL
BEAGLE (IL-28)
June
1936
DIMENSIONS
Wing
Span
Area
Aspect ratio
Overall length
Beight (gear daen)
Max diameter fuaelage
70.5 ft
670 sq ft
7.4
55 ft
20.5 ft
5.7 ft
POWER PLANT
No. & Modal
Type
Length
Diameter
Weight (dry)
(2) VK-1/VK-1A
Centrifugal
93 in.
50 in.
1900 lbs (VK-1)
2000 lbs
Exhaust Nozzle (Fixed)
360 sq. in.
Note: Later versions of 11-28 use
VK-1A engines.
WEIGHTS
Loading
Lb
Etpty
23,600
Take-off
Normal
1414,1400
Max
147,600
AMPR
16,800
ENGINE RATINGS
SL Static
lb
wc.#/hr/#.
(vic-1)
Take-off
6000
1.10
Nominal
5300
1.o6
Normal
48010
1.05
(vic-1A)
Take-off
7000
1.07
Nominal
6200
1.04
Normal
5600
1.02
GENERAL INFORMATION
General information only is quoted hereon. For more detailed information on
characteristics and performsmce see ATIC Study No. 102-AC-51/27-34, entitled
(Uncl) Analysio of Twin Jet Airplanes.
Engines are cantilever mounted forward of the wing leading edge.
Retractable tricycle landing gear. Main gear folds into engine nacelles.
Wings are tapered on trailing edge and straight on leading edge. Tips are
square. Slotted type flaps extend from the fuselage to the nacelle and from the
nacelle outboard approximately ten feet to the aileron.
It has a glassed-in nose for visual bombing.
A single bomb bay is located in the central part of the fuselage.
Defensive armament consists of two fixed guns, installed aide by side and
parallel to each other, under the flight deck, and a tail turret installation
similar to the US B-29 type. It Ls estimated that a range only fire control system
is installed.
A redone, housing blind bombing and navigation radar is located on the under-
side of the fuoelage.
The aircraft has been observed carrying wing tip tanka.
FUEL
Internal
External
lb
14,600
3000
Gallon
2200
440
BOMBS/FREIGHT
A bomb bay 14.0 ft long, 3.2 ft vide,
3.1 ft high at side wall and 3.4 ft
high at the centerline permits the
following bomb loads:
lb Type
Normal 4400 General purpose
(in combination)
For example:
2 FAB 1000 2200 lb ea 4400 lb total
4 FAB 500 1100 lb ea 4400 lb total
8 FAB 250 550 lb ea 4400 lb total
1 FAB 3000 6600 lb ea 6600 lb total
1 FAB 1500 3300 lb ea 3300 lb total.
27 FAB .100 220 lb ea 5940 lb total
Max 6600 lb with WW II types or im-
proved ballistic changes. (Max load .
.increase to 8800 lb highly probable.)
ELECTRONICS
Radar
Blind bombing and navigation similar
to US AN/APQ-13, nicknamed 'Mushroom'
IFF - SRO
Navigation
Radio compass - ARK-5
Radio altimeter, low - RV-2
Radio altimeter, high - similar to
US SCS-718
Distance measuring equipment -
Unknown type
Marker beacon - MIT-4812
Communication
VHF command radio - 4 channel-RSIU-314
MF/HF liaison radio - ART-13 and US-9
GUNS
Estimate 2
and 2 x 23
in nose of
Gun type
x 23 mm guns
mm fixed forward
fuselage
Cal
23-mm
in tail turret
firing gun
Cycle Auzzle
Rate Vel
'NR-23
800
2300
ROCKETS
None
,
,
HUM:50X1-
CONFIDENTIAL
O
it ?
CONFIDENTIAL
Juno
1936
BEAGLE (11-28 VK -1A)
AIRCRAFT PERFORMANCE
CONDITIONS
1
I
WO TT
11
I
go Tr
111
I
w TT
Ili
OPTIMUM
WO TT
OPT
W TT
TAKE-OFF WEIGHT
(lb)
(lb)
(lb)
(1b/ft2)
44,40o
14,600
4,400
66
46,600
14,600
6,600
69'
47,600
17,600
4,400
' 71
46,600
14,600
6,600
69
47,600
17,600
4,400
71
Fuel at 6.7 lb/gal
Payload (bombs)
Wing loading
Stall speed (power off)
(kn)
115
120
120
120
120
Take-off ground run at SL
(ft)
(1)
2,4-00
2,700
2,800
2,700
2,800
Take-off to clear 50 ft
(ft)
(1)
4,000
4,400
4,600
4,400
4,600
Rate of climb at SL
(fpm)
(1)
4,900
4,600
4,400
4,600
4,400
Time - SL to 20,000 ft
(min)
(1)
5.0
6.0
6.0
6.0
6.0
Time - SL to 30,000 ft
(min)
(1)
9.0
10.0
10.0
10.0
10.0
Service ceiling (100 fpm)
(rt)
(1)
43,603
42,500
41,900
42,500
41,900
COMBAT RANGE
(NM)
990
930
1,200
1,100
1,400
COMBAT RADIUS
(104)
510
495
615
6o5
745
Average cruise speed
(kn)
400
400
395
390
390
Initial cruising altitude
(ft)
39,300
38,300
37,300
40,400
39,000
Target speed
(kn)
(2)
410
410
405
395
395
Target altitude
(ft)
41,000
39,800
39,900
42,500
42,200
Total mission time
(hr)
2.50
2.50
3.00
3.00
4.00
COMBAT WEIGHT
(lb)
32,200
32,100
33,800
31,100
32,800
Combat altitude
(ft)
41,000
39,800
39,900
42,500
42,200
Combat speed
(kn)
(1)
440
445
440
44o
435
Combat ceiling (300 fpm)
(ft)
(1)
47,300
47,300
46,200
48,000
46,900
Service ceiling (100 fpm)
(rt)
(1)
50,000
50,200
48,900
50,800
49,500
Max rate of climb at SL
(fpm)
(1)
6,900
6,950 '
6,450
7,200
6,700
Max speed at 7,500 ft
(kn)
(1)
480
480
475
480
475
Max speed at 35,000 ft
(kn)
(1)
450
450
450
450
450
Max speed at optimum altitude
(kn/ft)
(1)
480/7000
480/7000
480/9000
480/7000
480/9000
LANDING WEIGHT
(lb)
28,000
28,000
28,400
26,500
26,800
,
-
.
NOTES
VK-1A engine rated at 7000 lb SLST
li Max power. (2) Normal rated power.
3 Missions X, II, and III are in accordance with Mil-05011A specs.
4), Missions IV and V are flown at the ceilfng for best NM/lb or limited to 100 fpm ceiling potential rate of
climb at Normal Power. Reserves permit 1/2 hour loiter at Sea Level with 1 engine operating.
(5) WO/TT . without tip tanks. W/TT ' with tip tanks.
ti
CONFIDENTIAL
50X1 -HUM
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
IL-28 (VK-1A)
6
5
CONFIDENTIAL
TAKE-OFF
Jam
'Anil I"
F
ip ip
CLEAR 50 Fr OBSTACLE
Er MEE "of

,F
4=I;
_L.
?krr
-
GROUND ROLL
T?
-14
Ii
Th-
+-
1
1
04t-
r-t
44#
1
1
4--
1111
?1-
1
11
4414-#4
1+1+
1
+1441111
28 32 36 40 44 48
GROSS WEIGHT - 1000 LBS
52
' -r
VK-IA ENGINE RATED AT
6000 LB SLST.
September
1855
60
56
0
040
0
IL
130
P20
?1
cr
10
SPEED
iii-
i I
?
-4?
'ifift
+hit
\-E4rT Lt
4 ?
? ?
444,
?
US
NM
,
T.O. WT. 44 ifi
4414-4-44
44,4
COMBAT W
"h
4,1-1
f#4. 44T-14-# rill It*
? MIL. PWR
NRP
.4.1
-11
-14
.04
-41
tit"
41
1'
rl-
.1!
I 1
14"1
?
-r-
I
4f4:
t-tt
1447
44
360 380 400 420 440 460 480
VELOCITY KNOTS
60
CLIMB
? ?4_
1 0 1:1 ELM
. : _
,4
COMBAT WT.
1.1
en
4
T. 0.? WT.
tt
MIL. PWR
NRP
1--
1
.44p-
rt-
I-
h-
0 I 2 3
4
5
RATE OF CLIMB - FT/MIN/1090
CONFIDENTIAL
6
7
50X1-HUM
?
January
1958
CONFIDENTIAL
BOSUN
REMARKS: BOSUN is a twin-jet Naval bomber designed by TUPOLEV. The Soviet designation of BOSUN
is TU-14.
SUMMARY
This aircraft was first seen in the July 1951 airshow at Tushino airfield in Moscow. It has been
in service use since 1951 and is now being replaced by the 11-28.
CONFIDENTIAL
50X1-HUM
ii
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
ARMAMENT ,
II
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
Type 35
Type 35
Mfc ne-igner. Tupolev
Type tight Bomber (probably Navy)
Crew 3
PERFORMANCE
March
1952
Maximum Speeds:
Cruising Speeds:
Climb: 4.5
Service Ceilings
Take-Off distanc
Fuel: (US gals.)
Combat Ceiling
467 knots t S.L.; 473 knots t 151300
Normal Power______knots a ft alt.
mins. to 15000 ft alt.; Rate of cli
: 43000 ft with normal weight;
e over 50 ft obstacle 397n
Internal: Hormel - 217 , Maximum
39,500
RANGES
ft alt.; 432 knots of 40000 ft cit.
; Economical knots t ft alt.
0: 3800 ft/min. at SL ft alt.
ft with lbs weight
ft into zero wind at See Level
; External: Normal Maximum
151n nautical
miles
2195 nautical
miles
nautical
miles
39s1 k no t 5,17cm-1p/inn ft
alt.
fuel
398 knots37500/470(1pft
alt.
fuel
knots,
ft
alt.
fuel
with 2/17 US gals, of
with 1075 US gals, of
with
US gals. of
and 4400 lbs bombs
and 0 lbs bombs
and
lbs
Combat Radius: 765
Combat Radius: 1040
POWER PLANT
No. 2
Type Jet
Description
rake-off 6onn
Normal 48n0
Military 60n0
War Emerg.
VK-1 Turbo,jet
lbs thrust, a
lbs thrust, e
lbs thrust, ?
lbs thrust, t
ft alt. 100% rpm
ft alt. 94, rpm
ft alt. 100% rpm
ft alt. rpm
knots
knots
knots
knots
1?2.11
Overall Dimensions: L:glifri
Net Dry Weight_ 2000 lba
Compressor Cen'rifugal typo
Compression Ratio 1 /CI
Type of Fuel Kerosene
SPECIFICATIONS
6.App?Y 50ins
Air HB5S Flow 1l0-115 approx.
Combustion Chambers 9
Turbine Stages 1
Ibs/sec
Specific Fuel Consumption 1.14 ;Approx.
(T.O., Sea Level, Static)
Guns 2,01mm Thu birrn+
ponlibly 2y2lnlin in nrIne.
section
Gunsight
BOMB/FREIGHT LOAD
Normal Load
Maximum Load
Loo
AAan
lbs
lbs
Bombsight
COMBAT PROTECTION
Armor
Fuel Tanks
SPECIFICATIONS
Materials
Span: 78 ft,____In; Length:_.64.ft,IL_In: height: ' ft,____in; Gross Wing Area 768 _sq.ft
Weights: Airframe lbs; Normal Gross /6000 ibs: Maximum Gross __lbs
ADDITIONAL DATA
The Type 35 is believed to be the operational model of 'the Type 12. The type 35 was first
seen at the July .51 Moscow Air Show in numbers,
CHARACTER! ST I CS C
COMM
CRAFT
50X1-HUM.
?
?
a
-
March
1952
500
PEED 8 04/MB
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MUM MEMAMM,amommmlinsmrammialsaaaannameimpss rempammmispaapammm
-3221)
mansimimmoramaisiniiiuiiuir nsammamaaaaawmanmanmasignmmunam
m imam
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4
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Omt22,2192:flatimmi
DESCRIPTION
(I) MILITARY POWER, GROSS WEIGHT 46,000 lbs.
(2) NORMAL POWER, GROSS WEIGHT 46,000 lbs.
? 8 5A 88 555 888
-q
50X1-HUM
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
SECRET
December
1957
BADGER
.?????
REMARKS: BADGER is a swept-wing, medium twin-jet bomber similar in configuration to the BISON
and is of TUPOLEV design. The Soviet designation is TU-16.
SUMMARY
This aircraft was first observed at KAZAN in 1953 and has been observed in numbers since 1955.
50X1 -HUM
SECRET
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
SECRET
BADGM
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
December
1957
DIMENSIONS
Wing
Span
Area
Aspect ratio
Cathedral
Sweepback
Inboard leading edge 42.0 deg
Outboard leading edge 37.0 deg
.Overall length 121.4 ft
Height, gear up 26.8 ft
Fuselage depth 8.5 ft
Fuselage width 8.0 ft
114 rt
2000 sq it
6.72
2.0 deg
POWER PLANT
No. & Model
Type
Length
Diameter
Weight (dry)
Exhaust Nozzle
(2) Mikulin AM-3AM
Axial-flow
18 ft
53 in
5500 lb
6.25 sq ft
WEIGHTS
Loading
lb
Empty
76,400
Takeoff
160,000
AlIER
52,500
ENGINE RATINGS
SL Static
Takeoff
Normal Power
lb SFC/#/hr/#
19,800 0.92
17,000 .89
GENERAL INFORMATION
Retractable tricycle landing gear with main gear housed in special nacelles.
,Wings are cranked at mid-span position. Two stall fences on each wing located
at half semi-span and at two-thirds semi-span.
The forward portion of the crew compartment consists of a flat windshield similar
to theUS 00-6 installation.
A single bomb bay is located in the fuselage extending equally forward and aft of
the wing trailing edge.
Defensive armament consists of three turrets located in upper forward, lower
forward and tail positions and a fixed forward firing nose gun.
Fire control for upper forward turret is provided from a top blister located
forward of the turret and behind the pilot; the lower turret is selectively
controlled from side blisters located directly aft of pilot and mid-way up side of
fuselage. Optical tail turret control is provided from inhabited gunner's station
similar to US B-29 type with apparent fire control radar redone of 18 inch
diameter over compartment with probable capability of search/track.
A large radome, suitable for blind bombing and navigation is located on the
underside of the fuselage below the canopy.
BADGER is equipped for aerial refuelirs; using a unique system incorporating a
hose connection between the wing nips of two BADGER aircraft.
FUEL
Internal
Weight, lb Gal
68,500 10,200
.For 10,000 lb design bomb load.
BOMBS/FREIGHT
A bomb bay 23.5 feet long, 5.25 feet
wide, and 4.3 feet high permits the
following bomb loads:
lb
Ncrmal 1700 to 20,000 Special Purp.
or
20,000 General Purp.
(in combination)
For example:
1 FAB 5000 11,000 lb ea 11,000 total
5 FAB 1000 2,200 lb ea 11,000 total
12 FAB 500 1,100 lb ea 13,200 total
36 FAB 250 550 lb ea 19,800 total
10,r.x 20,000 lb WWII or improved
ballistic shapes
ELECTRONICS
PADAR
IFF SRO Type
Tail Warning
Tail. Def. Search/Track
Range Only
Bomb Nay. W/Computer
PAVIOATION
D.R. Navigator
Radio Compass
Marker Beacon
Radio Altimeter
ILS, DIE, Rend. Beacon
Long Runge Nay Rcvr
Sun Compass
COMMUNICATIONS
HF, VHF
Intercom
GUNS
2 x 23 to 30 mm modified NR or high
performance type with cyclic rate from
800 to 1000 rpm guns in each turret al),
1 fixed MR 23 mm forward firing gun
right side of nose section.
ROCKETS
Hone .
1-HUM
SECRET
_
?
SECRET
December
1957
BADGER
AIRCRAFT
PERFORMANCE
CONDITIONS
Mission I4
Mission II4
Mission 1115
Mission IV5
TAKE-OFF WEIGHT
(lb)
160,000
160,000
16o,000
160,000
Fuel at 6.7 lb/gal
(lb)
68,500
75,500
60,soo
75,500
Payload (bombs)
(lb)
10,000
3,300
10,000
3;300
Wing loading
(lbisqft)
30
80
80
80
Stall speed (power off)
(kn)
110
110
110
110
Take-off ground run at SL
(ft)
(1)
4,600
4,600
4,600
4,600
Take-off to clear 50 ft
(ft)
(1)
7,000
7,000
7,000
7,000
Rate of climb at SL
(flla)
(1)
4,150
4,150
4,150
4,150
Time: SL to 35,600 ft
(min)
(1)
18.0
18.0
18.0
18.0
Service ceiling (100 fpm)
(ft)
(1)
40,400
4o,400
40,400
40,400
COMBAT RANGE
(1?14)
2,800
3,300
3,100
3,600
COMBAT RADIUS
(1111)
1,500
1,700
1,600
1,800
Average cruise speed
(kn)
465
465
465
465
Initial cruising altitude
(it)
35,600
35,600
35,600
35,600
Target speed
(kn)
(2)
475
475
475
475
Target altitude
(ft)
40,300
41,000
40,800
41,400
Final cruising altitude
(ft)
47,100
47,000
48,000
48,000
Total mission time
(hr)
6.5
7.5
7.0
8.0
COMIAT WEIGHT
(lb)
112,000
116,000
110,000
113,000
Combat altitude
(ft)
40,300
41,000
40,800
41,000
Combat speed
(kn)
(1)
490
490
490
490 ,
Combat rate of climb
(rpm)
(1)
800
800
. 800
800
Combat ceiling (500 fpm)
(rt) .
(1)
45,000
44,000
45,400
44,500
Service ceiling (100 fpm)
(ft)
(1)
48,300
47,600
48,000
48,100
Max rate of climb at SL
(rpm)
(1)
6,050
5,850
6,200
6,006
Max speed at opt altitude
(kn/ft)
(1)
,
550/13,200
550/13,200
550/13,200
550/13,200
Basic speed at 35,000 ft
(kn)
(1)
505
505
505
505,
TERMINAL TARGET ALTITUDE
(ft)
(1)
(3)
50,000 ,
51,500
50,000
. 51,500
.
.
,
'
'
NOTES ri
5
Maximum Power, AM-3AM engine rated at 19,800 lb SLST.
Normal Power.
50)(1 -HUM
Service Ceiling at maxim= power - with one hour fuel reserve for two engines ve,,a.a.15, pa... bomb load.
Missions I and II are in accordance with 14i1-C-5011A Speeification.
Missions III and IV are flown at the ceiling for best NM/lb or limited to 100 ft/min ceiling pot6ntial
rate of climb at normal power. Reserves permit one-half hour loiter at SL two-en ine-o eration.
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
SECRET
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
SECRET
TAKE-OFF
DISTANCE 1000 It)
T
L.
It
? ?
71-71-1111
CLEAR 50 FT
I 1 '
2
?
,
I 14-r 1.1i III)
Alt:
tia I**
II I * I
ilil
t lit.
tit itl, I:I
tlo 1,1,II
? ?11111111.111?Ell
1 I
.1,1
I
100 110 120 130 140 150 160 170 180 190
GROSS WEIGHT ( 1000 lb)
I I I
III
1._
II
4?L-11-11? I 1
I II,
1 1
r

?
4
J
1-1-1
t=
1 "1
II
I
1; 1-11-
I I.
tL
I. I
; ' ?
I 'IH
:1
,?
4:14-
1 i 1
?
IIIhHIHII
ME
NUM
MB
trf
44i4
December
1957
ALTITUDE ( 1000 ft)
50
40
30
SPEED
El
+,
? UM
MUM SMII MO
UR
J
JJLL1JiL LLL.L.t
MILITARY POWER
NORMAL RATED POWER III' 1111 Ili' t
?5 U
?a.
Mill
?r-
1 I r
wou Inrisimwr
? .114
117.11%1?1111
?
112,0040 LEIS:COMBAT WT
1-1-14- 11
fl
II
lit
1160,000 LBS T.O. WT
.4..1I LI1iJ IIHIM HIM
2O? PROBABLE STRUCT. LIMIT
450 KN EAS
1T3q11-1?
I II
1 441
10
SAKOMMII MUMMIKUM1111
umummusumnuu
mmumimmummumfiENI
'mum uumm mmuulailu u
REM? MAMMUMM SIM
NMI NMI
El
t-t-;
I
1
ammoub.
UMMMUMMISMNIIMM
1111111MUMMIII::
mummmun
0 III
450 460 470 480 490 500 ,510 520 530 540
ALTITUDE ( woo It.)
50
40
30
20
10
SL
KNOTS
CLIMB
III 11111 II I
IIIftIIIIIH
!!!! -I!!
:PINIn J.
1111
i
MILITARY POWER
NORMAL RATED POWER-- -
II
T 77:
-lit 4-
'
ME
MEN
NEM
-'-112,000LBS r. COMBAT WT
RIO ? I.
MIR
1:1:ft
160,000 Les 53)(1 -HUMWRIRIP: .,
. VII.drilirgi :1- , : I n t
1 _17 Nall$744111 111
- 1 hf:% I- '. ti-t-
, .
-1 - :
. -' i
1000 3000 50 00
RATE OF GLIMB-FT/M1N
SECRET
SECRET
December
1957
BISON
REMARKS: BISON is a swept-wing, four-engine, heavy jet bomber considered to have been designed
by MIASISCHEV. Two versions of this aircraft are in operation. The long nose version is presently in
production.
SUMMARY
This aircraft has been observed in numbers since 1955.
50X1 -HUM
SECRET
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
I
BISON
SECRET
December
1957
DIMENSIONS
Wing
Span
Area '
Aspect ratio
Cathedral
Sweepback
Inboard leading edge 41 deg
Outboard leading edge . 36:5 deg
Overall length (short rose) 155 ft
(long nose) 157 ft
Height, gear up 39 ft
Max diameter fuselage 11.5 ft
170 ft
3550 sq ft
8.1
3 deg
POWER PLANT
No. & Model
Type
Length
Diameter
Weight (dry)
Exhaust Nozzle
(4) Mikulin AM-3AM
Axial flow
18 ft
53 in
5500 lb
6.25 sq ft
WEIGHTS
Loading
lb
Empty
150,000
Takeoff
395,000
AMER
103,000
-
ENGINE RATINGS
SL Static thrust lbs SFC/#/hr/i
Takeoff 19,800
Normal Power 17,000
.92
.89
GENERAL INFORMATION
Retractable tandem gear installation; streamlined protuberance on each wing tip
estimated to house outrigger gear.
Wings are *cranked at mid-span position; a stall fence is located at about the two-
thirds semi-span position.
The forward portion of the creu compartment consists of a windshield similar to
the Vickers "Valiant" installation.
A single bomb bay is located in the fuselage extending to the mid-point of the
ying root from the trailing edge of the wing.
Defensive armament consists of three turret: located in upper forward, lower
forward and tail positions. Fire control for upper forward turret is provided
?from a top blister located forward of the turret and behind the pilot; the lower
turret is selectively controlled from side blisters located directly aft of pilot
and mid-way tp side of the fuselage. Optical tail turret control is provided from
inhabited gunner's station similar to US B-29 type With apparent fire control
radar radome of 18-inch diameter over compartment with probable capability of
search/track.
A large radome, suitable for blind bombing and navigation is located on the
underside of the fuselage below the canopy.
Two current configurations exist. Ohe has a short greenhouse bombardiers' nose
section and the other has a longer flush-mounted radar nose section. Both types
have detachable air-to-air refueling probes. The bomber aircraft has an alternate
mission as an aerial tanker through the use of a bomb bay conversion aerial
refueling package.
FUEL
I
Weight lb
gal
227,000 33,900
For 10,000 lb design bomb load.
BOMBS/FREIGHT
A bomb bay 20 feet long, 6
and 6.3 feet high permits
bomb loads:
lb
Normal 1700 to 30,000
or
20,000
(in
For example:
9 FAB 1000 2,200 lb an
24 FAD 500 1,100 lb ea
48 FAB 250 550 lb as
.7 feet wide
the following
Max 30,000 WWII type or
ballistic snapes
Type
Special Purp.
General Purp.
combination)
19,800 total
26,1400 total
29,700 total
improved
ELECTRONICS
RADAR
IFF SRO Type
Tail Warning
Tail Def. Search/Track
Rance Only
Bomb Nay. w/Computer
NAVIGATION
D. R. Navigator
Radio Compass
Marker Beacon
Radio Altimeter
ILS, DEE, Rend. Beacca
Long Range Nev. Rcvr
Sun Compass
COMMUNICATIONS
HF, VHF
? 1,
GUNS
2 x 23 to 30 as: modified NR or high
performance type with cyclic rate from -
(Soo to l000 rpm guns in each turret.
50X1 -I-
R (:) CKETS
None.
?
UM
SECRET
?
December
1957
SECRET
40111.1???1111???????????i.
BISON
AIRCRAFT PERFORMANCE
CONDITIONS
nission 14
Mission 114
Mission 1115
Mission IV5
TARE-OFF wiaGer
(1b)
(lb)
(lb)
(1b/8g ft)
(kn)
395,000
227,000
10,000
111
155
395,000
234,000
3,300
111
155
395,000
227,000
10,000
111
155
395,00?
234,000
3,300
111
155
Fuel at 6.7 lb/gal
Payload (bombs)
Wing loading
Stull speed (power off)
Take-Off ground run at SL
(ft)
(1)
7,700
7,700
7,700
7,700
Take-Off to clear 50 ft
(ft)
(1)
11,000
11,000
11,000
11,000
Rate of climb at SL
(fpm)
(1)
3,400
3,400
3,400
3,400
Time: SL to 20,000 ft
(min)
(1)
8.0
8.o
8.0
8.0
Service ceiling (100 fpm)
(ft)
(1)
37,200
37,200
37,200
37,200
Time: SL to 30,000 ft
(min)
(1)
15.0
15.0
15.0
15.0
COMBAT RANGE
(NM)
5,000
5,200
5,500
5,800
COMBAT RADIUS
(RM)
2,550
2,600
2,800
2,950
Average cruise speed
(kn)
450
450
450
450
Initial cruising altitude
(ft)
31,700
31,700
31,700
31,700
Target speed
(Mn)
(2)
460
460
460
460
Target altitude
(ft)
40,000
40,300
40,900
41,300
Final cruising altitude
(ft)
49,200
49,200
51,400
51,400
Total mission time
(hr)
11.5
11.5
12.5
13.0
COMBAT WEIGHT
(lb)
253,000
256,000
242,000
246,000
Combat altitude
(ft)
40,000
40,300
40,900
41,300
Combat speed
(Mn)
(1)
480
480
480
480
Combat rate of climb
(fpm)
(1)
900
800
. 900
800
Combat ceiling (500 fpm)
(ft)
(1)
_ 43,000
42,800
44,000
43,700
Service ceiling (100 fpm)
(ft)
(1)
46,600
46,300
47,700
47,300
Max rate of climb at SL
(fpm)
(1)
5,650
5,600
5)950
5,850
Max speed at optimum altitude
(kn)
(1)
530/18,000
530/18,000
530/18,000
530/18,000
Basic speed at 35,000 ft
(Mn)
(1)
.495
495
495
495
TERMINAL TARGET ALTITUDE
(ft)
(1) (3)
54,200
54,800
54,200
54,800
?
NOTES i211
5
Maximum Power, AM-3AM engines rated at 19,800 lb SLST.
Normal Power.
Service ceiling - with one hour fuel reserve for two engines operating, plus b(50X1-HUM
Missions I and II are in accordance with MIL-C-5011A Specification.
Missions III and IV are flown at the ceiling for best NM/lb or, limited to 100 ft/min ceiling potential
rate of climb at normal power. Reserves permit one-half hour loiter at SL, two-engine Operation.
SECRET
6
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
o
BISON
SECRET
DISTANCE ( 1000 ft )
12
10
TAKE-OFF
I I
PLWRIPIP1P1 ? ? 4..! ???1 ?:??
^ m m i RNU*Nl UI Ix _14:m lemma mmalli
11111111111111111?iiii Illiiillillii
IIHHIHH
Rini/1HW liii ill !ill
1111111111 21111111111111
. MMMMM OMMIUM MUMMODOMSRM 4pamammamamommmapi
8 1111111111111411111 "" " '
MENNIMMUMMERNMMEMM ouro UpgAMMEMEMEM am mmaa
^ NIONNIMS MEMMISMNSM ,da.mimmamplam:..ammai mm
? aledmarmIlln whIIIIHHHIH
riaturrowifiltraLl
6 1 1111M1101114h
^ mmmmm simmissmompng? ....migGROUNO ROLL MMAMM
mommimmamimppammaimmamam mum MEM
ammmitammaamap.mmmmamamia mmm ma mum WM
4 11111HOPHIHMUIP.7'n ,
!ER. 01141Bill 111.1111111 MINN HIH
^ NM NZ 11111maisUNUI
2 Keg maim
0 1111111111 1111 IIICHIIIIIIIIII
200 250 300
350
GROSS WEIGHT ( 1000 lb)
400
1
hu?
_t
LI
1
ALTITUDE ( 1000 It)
0
40
1111
SPEED
IMIMMMU MOON MUM MX
1111111111111 1111
mU
4_11+
-r
MIL PWR-- -7-
', NRP-------- =
NUN
In
RENVINURIO
MA
MUM
II
ammI rr
^ Ci
.4_4 H + +L-1+
44 2-5-6,000 LBS
H
maim 1NM..
IU am sam
-rT
RIM
4-1
Am:aka
? 744i
?
-r
CI I
0 T-395,000 LBS ? T.O. WT ,
? NW
111111MMMUNIS 11111
1011 .1.4ak MN
4+4-
I I
, ..
. MOM WM
10 ' , PROBABLE STRUCT. LIMIT
400 KN EAS
SL rt- ,IIIIIIIIIIIH
400 423 440 460 480 500 520
KNOTS
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SECRET -
-
'7?7
SECRET
December
1957
BEAR
REMARKS: SEAR is a swept-wing, four-engine turboprop heavy bomber considered to have been de-
signed by TUPOLEV. (Probable designation is TU-95.)
SUMMARY
Small numbers of these aircraft have been observed in fly-by practice for the May Day
Day Air Shows since April 1955.
SECRET
156).0 -H U M
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Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
SECRET
BEAR-
December
1957
DIMENSIONS
Wing
Span
Area
Aspect ratio
Cathedral
Sveepback
Inboard leading edge 40 deg
Outboard leading edge 36 deg
Overall length 150 ft
Fuselage diameter 9.5 ft
Height, gear up 33 ft
165 ft
2960 sq ft
8.7
2 deg
POWER PLANT
No. & Model
Type
Length
Diameter
Weight (dry)
Propeller
Type
No. blades
Diameter
Weight (assy)
(4) NK-12
Turboprop
(23.76 ft)
285 in. including
spinner and tailpipe
49 in
2800 lbs
Contra-rotating
8
18.4 ft
1700 lbs
WEIGHTS
,
Loading
lb
Empty
128,700
Take-off
300,000
AMPR
814, 000
ENGINE RATINGS
Sea level static Std. NACA Day
100% RAM efficiency
ESHP
SFC
RPM
ESHP
SFC
RPM
Take-off Power
12,100
.492 lb/hr/ESHP
8250
Normal Power
10,900
.50 1b/hr/HP
8000
GENERAL IN FORMATION
Engines are cantilever-mounted forward of the wing leading edge.
Retractable tricycle landing gear, with main gear housed in special nacelles
directly behind the inboard engines.
Wings are cranked near the outboard engine position. Two stall fences on
each wing at three-fifths and at four-fifths the semi-span.
The forward portion of the crew compartment consists of a flat windshield
similar to the US DC-6 installation.
A single bomb bay is centrally located in fuselage.
Defensive armament consists of two'dcfinite turrets identified and one
suggested turret; namely a tail turret, a lower aft turret, and a suggested lower
forward turret.
Fire control for fuselage turrets is expected to be remote optical sighting
stations resembling USAF B-29 equipment. A confirmed lower aft turret is control-
led by two blister stations located under the horizontal stabilizers, resembling
the Badger. An earlier estimate of a top upper forward turret and single blister
sighting station has been modified by a more recent sighting of a Bear with a
suggested lower forward turret and side sighting statiOn similar to the Bison
lover forward system. On the recent sighting there is no upper forward turret
position. Estimate that alternative defensive armament configurations are
currently being evaluated.
A large radome, suitable for .blind-bombing and navigation, is located on the
underside of the fuselage directly behind the optical bombsight window in the
nose section.
FUEL
Weight, lb Gal
150,000* 22,400
*For 10,000 lb design bomb load
BOMBS/FREIGHT
A bomb bay 24 ft long, 6 ft wide and 5.3
ft high permits the following loads:
lb Type
Normal 1700 to 22,000 Special
or purpose
20,000 General purpose
(in combination)
For example:
1 FAB 5000
20 FAB 500
42 FAB 250
11,000 lb ea 11,000 total
1,100 lb ea 22,000 total
550 lb ea 23,100 total
Max 30,000 lb WW II types or
improved ballistic shapes.
ELECTRONICS
Radar
IFF
Tail warning and fire control
Blind bombing and navigation
Navigation
Radio compass
Radio altimeter - high and low
Marker beacon receiver
Long range pnlse navigation receiver
VHF localizer receiver, DME
Communications
VHF command radio - 4 channels
MF - HF liaison radio
LF receiver
Intercom
GUNS
Estimate 2 x 23-to-30 mm guns per turret.
Identity cannot be confirmed. Photos and
supporting information suggest one of
the following types:
.Cyclic N5ox
Gun type . Cal Rate
Modified NR -23 23 mm 800 2000
Shch-3 23 mm 700 2300
Revolver type 23/30 mm 1000 3000/2400
ROCK E11 :3
1-HUM
SECRET
iv
1!
14
I
f11-9
:f
?
SECRET
December
1957
BEAR
AIRCRAFT PERFORMANCE
CONDITIONS
13113
Basic Mission
Basic Mission
1113
Optimum
14/?,n
10
Optimum
Mission
TAKE-OFF WEIGHT (lb)
300,000
300,000
300,000
300,000
Fuel at 6.7 lb/gal (lb)
150,000
157,000
150,000
157,000
Payload (Bombs) (lb)
10,000
3,000 .
10,000
3,000
Wing loading (psf)
-101
101
' 101
101
Stall speed (power off) (kn)
150
150
150
150
Take-off ground run at SL (ft) (1)
6,000
6,000
6,000
6,000 .
Take-off to clear 50 ft (ft) (1)
9,000
9,000
9,000
9,000
Rate of climb at SL (fpm) (1)
2,700
2,700
2,700
2,700
Time to cruise altitude (min)
25
25
32
32
Service ceiling (100 fpm) (ft) (1)
34,600
34,600
34,600
34,600
COMBAT RANGE (NM)
7,300
7,800
8,100
8,700
COMBAT RADIUS (UM)
3,800
3,950
4,200
4,400
Average cruising speed (kn)
450
420
405
405
Initial cruisins altitude (ft)
33,000
33,000
35,300
35,300
Target spe,d (kn)
435
435
410
410
Target altitude (ft)
39,000
40,100
41,900
42,300
Final cruising altitude (ft)
47,500
47,400
50,300
50,300
Total mission time (hr)
19
20
21
22
COMBAT WEIGHT (lb)
208,000
211,000
200,000
204,000
Combat altitude (ft)
40,000
40,300
42,100
42,500
Combat speed (kn) (1)
460
455
450
440
Combat rate of climb (fPril) (1)
550
500
400
.300
, Combat ceiling (500 fpm) (ft) (1)
4.0,600
443,200 .
' 41,200
40,900
Service ceiling (100 fpm) (ft) . (1)
43,900
43,500
44,500
44,100
Max rate of climb at SL (fpm) (1)
4,350
4,300
. 4,550
4,450
Max speed at optimum altitude (kn/ft) (1)
495/21,400
495/21,300
495/21,600
495/21,500
Basic speed at 35,332 ft (kn) (1)
47o
470
475
475
TERMINAL TARGET ALTITUDE (ft) (5)
50,000
51,000
50,000
51,000
(ft) . (6)
48,900
.
,
NOTES (1) Take-off power. , (2) Nortal power.
(3) Missions I and II are in accordance with Mil-C-5011A specification.
(4) Missions III and IV are flown at the ceiling for best NM/lb or limited to 100 '/Min ceiling potential rate
of cliAb at normal power. Reserves permit one-half hour loiter at S.L., two-engine operation.
(5) Service ceiling at Max. Pwr. with one hour reserves taus bomb load. No range figure is associated with
this altitude.
(6) This altitude is for a bomb load of 20,000 lbs.
SECRET
50X1 -HUM
I
I I
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
SECRET
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
December
1957
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SECRET
114
,
11
SECRET
November
1956
BLOWLAMP
REMARKS: BLOWLAMP is a twin-jet, swept-wing light bomber claimed by the Soviets to be capable
of supersonic performance.* Believed to be the replacement for BEAGLE (I1-28) aircraft, it is classed
as a high performance weapon of considerable versatility and growth potential.
1956 First observed during rehearsals for the Aviation Day Air Show.
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
;..
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
_
Ii
SECRET
BEAR
9
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SECRET -
SECRET
November
1956
BLOWLAMP
REMARKS: BLOWLAMP is a'tirin-jet, swept-wing light bomber claimed by the Soviets to be capable
of supersonic performance.* Believed to be the replacement for BEAGLE (IL-28) aircraft, it is classed
as a high performance weapon of considerable versatility and growth potential.
*See General Information
SUMMARY
1956 First observed during rehearsals for the Aviation Day Air Show.
50X1-HUM
SECRET
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
SECRET
BLOWLAMP
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
November
1956
DIMENSIONS
Wing
Span
Area
Aspect Ratio
Cathedral
Sweepback
Inboard leading edge
Outboard leading edge
Overall length
Height gear up
Fuselage depth
Fuselage width
54.9 ft
685 sq ft
4.4
3.5 deg
55 deg
52.5 deg
71 ft
18 ft
7.1 ft
5.3 ft
POWER PLANT
No. & Model
Type
Length
Diameter
Weight (dry)
Exhaust Nozzle
Diameter
(2)
Axial-flow turbojet
140 inches
40.25 inches
2,900 lb
23 inches
WEIGHTS
Loading
lbs
Empty
29,920
Tale-off
Design
56,100
Normal
59,400
Overload
60,500
AMPR
21,500
ENGINE RATINGS
SL Static
Max
lb SFC/f/hr/#
11,600 .92
GENERAL INFORMATION
It should be noted that the above dimensions and engine data are the ones on
which the performance figures are based. However, these dimensions and engine
data are approximations only, and are subject to Change upon receipt of confirmed
information. When such information is available and reflects changes of suffi-
cient magnitude, the performance will be revised accordingly.
Engines are installed in pylon-mounted nacelles.
The wings are cranked at the engine pylcn position. Two stall fences on each
wing are located at the cranked position and at the aileron-flap junction.
Retractable tandem main landing gear with outrigger gear housed in wing tip pods.
A small single bomb bay is centrally located in the fuselage.
Defensive armament consists of two fixed forward firing nose guns and an optical
tail turret which contains two guns. Fire control of the turret is provided from
the inhabited gunner's station similar to the BEAGLE. Radar and possibly IR
equipment is installed to provide detection and ranging information for the
defensive fire control function.
A radome suitable for blind bombing and navigation is located between the bomb
bay and the forward gear door.
The presence of an instrumentation boom in the nose suggests the aircraft
observed is in prototype status.
The design does not reveal aerodynamic characteristics commensurate with super-
sonic performance capability claimed by the Soviets. However, it does suggest
fairly high subsonic speed performance. It is estimated that in a dive from an
altitude of at least 40,000 ft, BLOWLAI0, can flash through the 35,000 ft altitude
at speeds slightly in excess of Mach 1.3 but cannot stabilize at this speed in
level flight.
FUEL
Weight lb Gal
Internal 20,000 3,000
BOMBS/FREIGHT
A bomb bay 11.5 feet long, 4.5 feet
wide, and 4.5 feet high permits the
following bomb loads.
lb Type
Design 1500 Special Purpose
Normal 6600 General Pumps,
Maximum 7700 General Purpose
(In combination)
For example:
12 250 Kg ea 6600 lb total
2 1500 Kg ea 6600 lb total
1 3000 Kg ea 6600 lb total
(In combination)
6 25o Kg ea
plus
4 500 Kg ea 7700 lb total
ELECTRONICS
IFF, SRO (Identification Friend or Foe)
Bombing-Navigation Radar, MUSHROOM
Tail Defense Radar, Range-Only Type
Radar Warning Receiver
ILS Localizer Receiver (KRP-F)
Low Level Radio Altimeter (RV-2)
Distance Measuring Equipment (SD-1)
Marker Beacon Receiver (MRP-48P)
Low Frequency Navigation Receiver (MOON)
Short Range Precision Navigation
Receiver (SEORDIALK)
VHF Command Trans/Rec RSIU-3M (100 to
150 Mc)
EF Liaison Transmitter, Version of US
AN/ART-13 (2 to 12 Mc)
HF Liaison Rec. US-9 (2 to 12 Mc)_
Intercom Amplifier SPU-2
GUNS
4 x 23 an with cyclic rate up to
1200 rds/min
2-revolver type fixed in nose forward
firing
2-SHCHA or revolver type in tail turret
ROCKETS
50X1 -HUM
SECRET
?
?
1
November
1956
SECRET
BLOWLAMP
AIRCRAFT PERFORMANCE
CONDITIONS
13
Basic Mission
1'3
Basic Mission
III4
Opt. Mission
1v4
Opt. Mission
TAKE-OFF WEI= (lb)
56,100
59,400
56,100
59,400
Fuel at 6.7 lb/gal (lb)
20,000
20,000
20,000
20,000
Payload (bombs) (lb)
3,300
6,600
3,300
6,600
Wing loading (lb/sqf(.)
81
86
81
86
Stall speed (power off) (kts)
155
160
155
160
Take-off ground run at SL (ft)
3,600
4,100
3,600
4,100
Take-off to clear 50 ft (ft)
5,600
6,300
5,600
6,300
Rate of climb at SL (fizz)
9,500
8,900
9,500
8,900
Time: SL to 35,000 ft (min)
5.8
6.2
5.8
6.2
Service ceiling (100 fpm) (ft)
44,400
43,100
44,400
43,100
COMBAT RANGE (KM)
1,550
1,450
1,700
1,580
COMBAT RADIUS (NM)
800
775
870
845
Average cruise speed (kts)
490
490
490
490
Initial cruising altitude (rt)
38,800
37,200
38,800
37,200
Target speed (kts) (2)
500
500
500
500
Target altitude (ft)
45,640
44,400
45,900
44,600
Final cruising altitude (ft)
46,300
46,300
46,900
46,900
Total mission time (hr)
3.3
3.2
3.6
3.4
COMBAT WEIGHT (lb)
42,400
42,200
41,800
41,600
Combat altitude (ft) (1)
45,600
44,400
45,900
44,600
Combat speed (kts)(1)
535
535
535
535
Combat rate of climb (fpm)(1)
I,600
2,000
1,600
2,000
Combat ceiling (500 fps) (ft) (1)
48,900
49,000
49;000
49,000
Service ceiling (100 fpn) (ft) (1)
50,000
50,100 ,
50,400
50,500
Max rate of Climb at SL (Tpo)(1)
12,400
22,506
12,600
12,700
-Max speed at optimum altitude (kts)(1)
615/SL
615/SL
615/SL
615/SL
Basic speed at 35,000 ft (kts)(1)
545
. 545
545
545
?
NOTES (1) Military power.
(2) Normal power.
(3) These midsions are in accordance with mil-c-50liA.
(4) Missions III and IV are flown at the ceiling for best NM/lb or limited to 100 ft/min ceiling 'potential
rate of climb at normal power. Reserves permit one-half hour loiter at SI, two-engine operation.
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
SECRET
50X1 -HUM
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Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
? ?
? ?
? ?
SECRET
January
1958
BACKFIN
REMARKS: BACKFIN is a supersonic, swept-wing twin-jet light bomber.
SUMMARY
1957 First observed in the eighth rehearsal of Tushino airshow.
50X1 -HUM
SECRET
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SECRET
BACKFIN
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
January
1958
DIMENSIONS
Wing
Span
Area
Aspect ratio
Sweep back
Inboard leading edge 57.5
Outboard leading edge 54
Over-all length 104
Height, gear up 23.6
Fuselage
Depth
Length
Width
62 ft
950 sq ft
4.05
deg
deg
ft
ft
8.4 ft
ft
ft
87
10
POWER PLANT
No. & Model
Type
Length
Diameter
Weight (dry)
(2)
Axial flow turbojet
with afterburner
269 in.
43 in.
5000 lb
WEIGHTS
Loading
lb
Empty
143,000
Take-off
86,000
Useful load
143,000
AMPR
28,000
ENGINE RATINGS
SL Static
Max
Mil
lb
21,000
15,900
SFC
1.92
.92
GENERAL INFORMATION
Wings are highly swept, cranked, in the low-mid position.
Engine inlets are mounted high on and apart from fuselage sides, yell ahead
of wing leading edge. The two engines are probably located in the vicinity of,
and above the wing root section.
The fuselage is deep in the mid section, flattened on the underside similar
to the B-58 and tapers sharply upward to the twin exhaust section. A large crew
compartment is set atop the fuselage similar to the B-58.
The swept-back empennage assembly consists of a low horizontal tail mounted
below the exhaust section, and a large high-aspect-ratio vertical tail.
The configuration suggests that a tandem type landing gear is used.
Fire control for the rear defensive armament is probably by remote radar
operation from the flight deck.
The large size of the efflux indicates the installation of high-thrust
engines with afterburners.
The general appearance of the aircraft is consistent with a supersonic
speed capability.
FUEL
Internal
Weight, lb Gal
35)000 5,400
BOMBS/FREIGHT
Bomb bay
Length
Width
Depth
Maximum bomb load
15 ft
5 ft
4.5 ft
15,000 lb
ELECTRONICS
Radar
MUSHROOM (Bombing-navigation radar)
IFF
ECM
Tail defense
Navigation
SHOREWALK (Short range navigation sys)
MOON (Long range navigation sys)
Radio compass
ILS
Localizer and glide path receiver
Marker beacon equipment
DME
Radio altimeter
Communications
VHF transmitter-receiver (4 or 8 chan)
HF transmitter-receiver
Intercom
GUNS
2 x 23 mm with cyclic rate of 1000
rds/min and 500 rds each in tail
turret.
50X1 -HUM
SECRET
1.
?
?
SECRET
January
1
BACKFIN
AIRCRAFT PERFORMANCE
CONDITIONS
SUBSONIC
MISSION
SUBSONIC MISSION (opt)
Mach- 1.06
ZONE MISSION
Mach- 1.06
WEE MISSION
(opt)
TAKE-OFF WEIGHT
(lb)
86,000
86,oco
86,000
86,000
Fuel at 6.7 lb/gal
(lb)
35,000
35,000
35,000
35,000 ,
Payload (Scabs)
(lb) (7)
6,600
. 6,600
6,600
6,600
Wing loading
(lb/sq ft)
88
88
88
88
Stall speed, clean (power off)
(kn)
160
160
160
160
Take-off ground run at SL
(ft)
3,000
3,000
3,000
3,000
Take-off distance to clear 50 ft
(ft)
5,600
5,600
5,600
5,600
Rate of climb at SL
(rpm) (2)
6,600
6,600
6,600
6,600
Time: SL to 20,000 ft
(min) (2)
3.3
3.3
3.3
3.3
Service ceiling (100 Ppm)
(ft) (2)
42,600
42,600
42,600
42,600
Time: SL to 30,000 ft
(min) (2)
5.7
5.7
5.7
5.7
COMBAT RANGE
(101)
1,900
2,100
1,500
(5)
1,600 (5)
COMBAT RADIUS
(NM)
1,000
1,100
800
(6)
9oo (6)
Average cruise speed
(kn)
520
520
520
520
Initial cruise altitude
(ft)
39,600
39,600
39,600
39,600
Target speed
(kn)
530
(3)
530
(3)
610
(1)
610 (1)
Target altitude
(ft)
43,000
43,300
42,500
43,000
Final cruise altitude
(ft)
50,200
51,000
50,200
51,000
Total mission time
(hr)
3.9
4.2
3.5
3.8
CCMBAT WEIGHT
(lb)
59,500
58,300
58,700
57,600
Combat altitude
(ft)
43,000
43,300
42,500
43,000
Combat speed
(kn)
555
(2)
555
(2)
610
(1)
610 (1)
Combat rate of climb
(rpm) (2)
2,000
2,100
2,200
2,200
Combat ceiling (500 fpm)
(ft) (2)
48,700
49,100
49,000
49,400
Service ceiling (100 fpm)
(ft) (2)
50,400
50,800
50,700
51,000 '
Max rate of climb at SL
(fpm) (2)
10,600
10,900
10,800
'
11,000
Max speed at opt altitude
(kn/ft) (1)
705/35,000
705/35;000
705/35,000
705/35,000
TERMINAL TARGET ALTITUDE
(ft) (2)(4)
52,800
52,803
,60,000
60,000
.
_
-
.
NOTES
Maximum power (2) Military power (3) Normal rated power
Service ceiling: Half hour fuel reserves Plus bomb load
Includes 100 NM dash at Mach 1.06
Includes 50 NM dash at Mach 1.06
Same performance with either 3,300 or 6,600 lb bomb load. No additional fuel carried with 3,300 lb
bomb load as aircraft is fuel volume limited.
50X1 -HUM
SECRET
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Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
It is a strut-braced high-wing monoplane vith strut-braced tail assembly and fixed main
vheels and tail vheel. Streamline fairings fitted on in wheels.
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
? CONFIDENTIAL
Yak-12
Yak -.12
Mfr Designer: Yakovlev Crew 1
Type Liaison, Communication, Transport
PERFORMANCE
July
1953
Maximum Speeds. 110 knots a S.L.;
knots e
ft alt.;
knots a ft alt.
Cruising Speeds:
1.2
Normal Power
knots
ft alt.;
a . ft
alt.; Economical
Climb.' 848
'75
knots a SL ft alt.
plos, to 1000
Rate of
normal weight;
ft/min. at SL ft alt.
.Climb:
Service Ceilings:
ft
with
ft with lbs weight
Take-Off distance
over 50 ft obstacle
350
ft
into zero wind at Sea Level
Fuel: (US gals.)
Internal: Normal
40
Maximum
; External:
Normal
. Maximum
,
RANGES
420
nautical miles
210
nautical miles
nautical miles
? knots,
5000 ft alt.
it
75 knots,
5000 ft alt.
knots, ft alt.
wTTI5R-1-
US gals, of fuel
with
25
US gals, of fuel
with
US gals, of fuel
and 3 lbs passengers
4 lbs
aod
lbs
and
passengers
Combat Radius: 225 naut. mi.
Combat Radius: 120 naut. mi.
POWER PLANT
No. Engines
1 Take-Off 145 hp. 0 SL ft alt.__110 rpm in. 111.
Normal hp e ft alt.
rpm in. Ng.
Type Engines Reciprocating military
135 hp. e SL
:: aalit: rpm in. Ng. 1740 rpm in. Ng.
War Emergency hp. e
Description
M-11F, 5 cylinder, direct drive, air-cooled radial.
SPECIFICATIONS
SUPERCHARGER
Bore 4.9 Ins Dry Wt. 352 No. Speeds None Mfr.
Stroke 5-5 Ins Red.Gear No. Stages
Displ 525 Cu. ins Eng.Width 42.2 in. Ratios
Comp. Ratio Eng.Leingth 17.4 in. Impeller Dia ins Pitch Control
PROPELLER FUEL
No.Blades 2
Dia. ft,
Ins
Type Gasoline
70 Octane
ARMAMENT
BOMB/FREIGHT LOAD
COMBAT PROTECTION
'Guns None
Normal Load .200 lbs
Armor None
Maximum Load 600 lbs
.
Freight load or 3 or 4 passengers
.
.
.
Gunsight
Bombsight
Fuel Tanks ?
.
ISPECIFICATIONS
Materials Mixed wood-and metal construction: . ? ?
Span:39 ft,6 In; Length:21___ft,_?_ln: Height. ft, In; Gross Wing Area 237
Weights: Airframe 950 lbs; Normal Gross* 2650 lbs: Maximum Gross
sq. ft
lbs
ADDITIONAL DATA
. Brought into use after World War II as a civil transport and limited use as a military
aircraft. It is not known how many of these have been produced but it is believed to be in
rather extensive use..
? CONFIDENTIAL,
50X1-HUM
July
U. S. S. R.
1953
CONFIDENTIAL
?
Iv.NI
An-2
An-2
DESCRIPTION
This aircraft is a biplane. It has fixed main gear and tail wheel. It is a cabin type,
single engine aircraft equipped with a four bladed scimitar pattern propeller. This aircraft
will probably be used as a replacement for the Po-2 on local runs and feeder lines.
CONFIDENTIAL
50X1-HUM
1
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
An-2
CONFIDENTIAL
An-2
IMfr. , Designer: Antonov
Type Light Transport
Crew
PERFORMANCE
July
1953
Noximum SOcads: 132 knots a S.L.; 138 knots 41 5000 ft alt.;knots e
Cruising Speeds: Normal Power knots I ft alt.; Economical knot; e
Climb: 1? mins. to 10000 ft alt.; Rate of Climb; 770 ft/min. at
Service Ceilings; 15000 ft with normal weight; 13000 ft with 13000
Take-Off distance over 50 ft obstacle 1470
Fuel: (us gals.) Internal: Normal 370 , Maximum . External; Normal ,
ft alt.
5000 ft alt.
SL ft alt.
lbs weight
ft into zero wind at Sea Level
Maximum
RANGES
853
nautical
miles
alt.
fuel
nautical
miles
alt.
fuel
nautical
miles
alt.
fuel
? 06 knots,
5000 ft
?
knots,
ft
?
knots,
ft
with 170
US gals. of
Cargo
with
US gals, of
with
US gals, of
and 4200 lbs
and
lbs
and
lbs
Combat Radius: 440 Nautical Miles
POWER PLANT
No. Engines I Take-Off 985 hp. e SL
Normal 839 p. s 5000
Type Engines NeciProcatingMilltary hp. ?
Mar Emergency hp. e
Description ASh-82-IR, 9-cylinaer, air-cooled radial engine
ft alt 2200
ftalt. am
ft alt.
ft alt.
rpm
rpm
rpm
rpm
in. Hg.
In. HO.
In. Hg.
In. Ng.
SPECIFICATIONS
Bore 6.125 ins
Stroke6.870 ins
Oise!. 1822 cu. ins
Comp. Ratio 6:_1_
SUPERCHARGER
Dry Wt. 1246 (Instio. Speeds 1
Red.Gear 11:16 No. Stages 1
Eng.Width 55 Ratios 7:1
Eng. Length 44.79 Impeller Dla10.0 Ins
Mfr.
PROPELLER
Ho. Blades
It
Dia. ft, Ins
Pitch Control
FUEL
Type 95/115
Probably automatin
BOMB/FREIGHT LOAD
COMBAT PROTECTION
Guns
None
Normal Load
4200 lbs
Armor
None
Maximum Load
5000 lbs
14 .passengers
GunsIght
None
Boxibsight
None
Fuel
Tanks
Noun
.
SPECIFICATIONS
Materials Mixed construction
Spae:Ja_ft,_ilin; Length:_r_ft,_Zia; Height'
Weights: Airframe lbs; Normal Gross
ft,
' 12200 lbs; Maximum Gross
in? Gross Wing Area
990
13000
sq. ft
lbs
ADDITIONAL DATA
This aircraft was first observed in July 1948 in the Aviation Day
sequently reappeared in July 1951 in the Aviation Day air show. Since
observed in Poland and is believed stationed at Warsaw.
The An-2 is reported to have a cargo loading door large enough to
design of the aircraft appears to lend itself to service, as a light tr
observation/reconnaissance plane, or trainer. It is likely to be used
bush-type transport in underdeveloped areas.
air show at Tushino. It sub-
that time the An-2 has been
accommodate litter cases. The
ansport, ambulance aircraft, '
in a feeder-line role and as a
CONFIDENTIAL
?
50X1-HUM
-r
July
U.S.S.R. 1
1953
ALTITUDE (FT)
26000
24000
22000
20000
16000
14000
12000
10000
8000
6000
4000
2000
CONFIDENTIAL
An-2
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TIME TO.CLIM13 (MIN)
FeliMMOIMICE
DESCRIPTION
Normal rated power, normal gross weight.
CONFIDENTIAL
50X1-HUM
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
I DESCRIPTION
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
An-2
U.S.S R.
DISTANCE (FT)
1800
1600
1400
1200
1000
800
CONFIDENTIAL
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1953
l_atmott=L-1
CONFIDENTIAL
50X1 -HUM
or>,
January
1958
CONFIDENTIAL
CAB
REMARKS: Soviet designation of this aircraft is Li-2.
SUMMARY
CAB is a twin-engined, low-wing monoplane built under license in the USSR. It is no longer in
production but is still in extensive use both as a civil and military transport.
50X1 -HUM
CONFIDENTIAL
,01.1.???????????????????
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
CONFIDENTIAL
CAB
January
1958
DIMENSIONS
Wing
Span 94.5 ft
Area 985 sq ft
Fuselage length 64.4 ft
Height (Horizontal
attitude) 23.3 ft
Cargo cabin
Length 30.9 ft
Width (max) 7.68 ft
Height (max) 6.5 ft
Usable volume 1310 Cu ft
POWER PLANT
No. & Model
Type
2 x Ash-62IR
9 cylinder, single
row, air-cooled
radial
Propellers 2-AV-7N-161; three-
bladed, 11.8 ft dia
WEIGHTS
Take-off
lb
Normal
25,300
Max allowable
26,400
Empty
15,350
ENGINE RATINGS
Take-off 985 BHP at 2200 RPM,
41 in. Hg
Normal 830 BHP at 2100 RPM,
35 in. Hg at 4,900 ft
GENERAL INFORMATION
CAB is the Soviet model of the U.S. DC-3 built under license. The Soviet
aircraft designer LISITSIN is given credit for this design in the USSR. The
major difference frpm the U.S. 00-3 is the engine.
.Alternate variants of CAB will carry up to 19 passengers or 25 paratroops.
FUEL
Gal
Type 95/115
4930 lb 822
BOMBS/FREIGHT
Cargo
Normal 3,300 lb
Maximum 6,600 lb
(Limited by floor strength)
ELECTRONICS
Radio compass
IFF
VHF command set (4 channel)
HF liaison set
Interphone
Localizer
Glide path
Marker beacon receiver
CREW
Pilot. '
Co-Pilot
Navigator
Radio operator
50X1 -HUM
CONFIDENTIAL
CONFIDENTIAL
January
1958
CAB
AIRCRAFT PERFORMANCE
CODINS
N TIO
M
ONOMICAL CRUI SF
MAXIMUM
CARGO
LONG
RANGE
SL
10,000 ft
15,000 ft
TAKE-OFF WEIGHT (lb)
25,300
4,900
3,300
25.7
60
25,300
4,900
3,300
25.7
6o
25,300
4,900
3,300
25.7
6o
25,300
1,600
6,600
25.7
Eo
25,300
4,900
3,300
25.7
Co
Fuel weight (lb)
Payload (cargo) (lb)
Wing loading (lb/8g ft)
Stall speed (km)
Take-off run - SL (ft) (1)
1,350
1,350
1,350
1,350
1,350
Take-off distance - (ft) (1)
3,000
3,000
3,000
3,000
3,000
50 ft obst
Rate of climb - Si, (ftimin)(2)
700
700
700
700
700
Time: SL to 5,000 ft (min) (2)
NA
7
7
NA
7
Time: SL to 10,000 ft (min) (2)
NA
NA
17
NA
17
Service ceiling (ft) (2)
16,600
16,600
16,600
16,600
16,600
COMBAT RANGE (NM)
1,080
1,140
1,175
345
1,215
Average speed (km)
120
130
130
120
130
Cruise altitude (constant) (ft)
SL
5,000
10,000
SL
13,000
Mission time (hr)
9.0
8.8
9.2
2.9
9.4
COMBAT RADIUS (NM)
510
525
535
135
530
Average speed (KO
120
130
130
120
130
Cruise altitude (ft)
SL
5,000
10,003
SL
13,000
Mission tim..1 (hr)
8.5
8.1
8.3
2.3
8.2
FIRST LANDING WEIGHT (lb)
23,100
23,200
23,300
24,500
23,500
,
,
NOTES (1) Maximum power
(2) Normal power
50X1 -HUM
CONFIDENTIAL
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Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
e
Low-wing, twin-engine monoplane with single fin and rudder, and retractable
landing gear.
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Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
Yak-16
CONFIDENTIAL
Yak-16
mfr.
Type
Designer: Yakovlev
Light Transport
Crew 3
Maximum Speeds; 200 knots a S.L., 208
Cruising Speeds; Normal Power 187 knots
Climb: 10 mins. to 10000 ft a
Service Ceilings: ft with
Take-Off distance over 50 ft obstacle
Fuel: (US gals.) Internal: Normal 275
PERFORMANCE
July
1953
knots e 6000 ft alt.:___17SL?knots 6 15000 ft alt.' I
r 10500 ft alt.: Economical 150 knots q 10500 ft alt.
It.; Rate of Climb; 12 0 ft/min. at SL ft alt.
normal weight; 16000 ft with 14100 lbs weight
1550 ft into zero wind at Sea Level
, Maximum ; External; Normal , Maximum
RANGES
575 nautical miles
siL,52knots, 10000 ft alt.
with 275 US gals. of fuel
and 1000 lbs freight
Combat Radius: 260 Nautical Miles
with
and
nautical miles
knots, ft alt.
US gels. of fuel
lbs
POWER PLANT
nautical miles
knots, ft alt.
with US gals, of fuel
and lbs
No. Engines 2 Take-Off
Normal
Type Engines Recinrocatingmilitary
War Emergency
690
hp. fp
592 hp. p 66co
hp. ?
hp. a
SL ft alt. 2500 rpm in. Ht.
ft alt. 2400 rpm In. HP.
ft alt. rpm In. Hg.
ft alt. rpm in. Hg.
Description ASh-21 7-cylinder, air-cooled radial engine
SPECIFICATIONS
Bore 6.12 ins
Stroke6.12 .In
Disp1.1260 cu.ins
Comp. Ratio_6-6:_l_
SUPERCHARGER
PROPELLER
FUEL
Dry Wt. 1077 No. Speeds 1 Mfr. Visch 111-V-120 Type 89 Octane
Red. Gear 11:16 No. Stages 1 No.Blades 2 solid dural
Eng.Width 49.5 Ratios 711 Dia. 9 ft, 7 ins
Eng.Length 5 Impeller Dia 9.69ins Pitch Control R-7# goy constant sneed
ARMAMENT
Guns None
Gunsight N..c
BOMB/FREIGHT LOAD
Normal Load 2500
Maximum Load 3000
Alternate marimum
lbs
lbs
10 passengers and
440 lbs freight or
3000 lbs freight or
13 troops
Bolabsight
None
SPECIFICATIONS
Armor
COMBAT PROTECTION
None
Fuel Tanks None
Materials All metal construction
Span:iiLft,___In; Length: 46 ft,___In; Height:_12._ft, in; Gross Wing Area 600
Weights: Airframe lbs; Normal Gross lbs: MaXIMUM Gross 14100
sq. ft
lbs
,ADDITIONAL DATA
, This is one of the latest Soviet transports designed for feeder-line duties. It appeared in
1948. This aircraft is an intermediate type between the Yak-6 and Li-2 or 11-12. It will probably
be used mainly as a civil type. It is equipped with a radio compass and a transmitter/receiver.
CONFIDENTIAL
50X1 HUM
0
CONFIDENTIAL
March
1952
ALTITUDE -FT
30,000
25 000
20 000
15 000
10-1:1114.
5 000
S.L.
SPEED If CL /418
11
11111 111111m
m1111111:111111111111_
111111111pri
MINION 4111111 4110111U
!ull11111111111111111111111
? II
UIIHIHIIifi
minommumusmsam
immummummmmummummunsimil annum
immummmounsmummamm immumummommo
ERMENNIMENEMMEM
I ?
111111111111111
Imummiumummummilmommimm mom
._Mt...miammintliMMMOMMIIMMUMMEMIN
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NM IMMIMMEMMMENEMINMax speed
MEVEXMOMMOMEMMINMEMMEMMEMMOMMAIMMIMME
MEXIMIMUMMOMMUMENEMMIIMMENM.M.MMIX
EM LTime to climb MMINMEMENMERNWOMUMMIMMUMMIMILVENNUM
INEWANNIMUMERMUMORMIMUNUMUUMMIUMMIMMEMMIMMUU
looFT/humr
SPEED?KNOTS 1
0
MIM TO CLIMB I
0
4
6
8
10
12
100
200
300 400
500 600
10
20
30 40
50
m-3.6
L_ImazamacxJ
DESCRIPTION
Normal rated power, maximum gross weight.
CONFIDENTIAL
50X1-HUM
Mem
551 IS In art - anitize
rove or e ease
PPRPOv vim 1
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
A
YAK-16
CONFIDENTIAL
U.S.S.R.
OBSTACLE- FT.
18bu
1700
1600
cr.
U1
1400
1300
1200
U.
U.
I 1100
1000
GROSS WT 1000 LBS
TAKE -OFF
CONCRETE RUNWAY
--- TURF RUNWAY
11
/11
12
13
INSIX
MEE
II
NNW MN
XXX
11
14
11
_L
II
XXX
mu
Nam
15
16
March
1952
I DESCRIPTION
CONFIDENTIAL
VPS:terlh
50X1 -HUM
-- -4-,77,..f,,,. -=-.1-..,.....--.7,1--z,,:-%,-,,,,..........-........r..............---- - ........--.., ,-..
ri
CONFIDENTIAL
July
1953
U. S S. R.
11-12
. .
_
- DBC- ? 6, -6
IL-12
DESCRIPTION
This is a twin-engine, low-wing, monoplane transport. It has a single tail and retractable
tricycle landing gear. The in wheels are dual, retracting into the engine nacelles and the nose
wheel is single, retracting aft. The wing has upward dihedral; the center section in of rectangular
shape, while the outer sections are trapezoidal with rounded tips. Split landing 'ISA
1M
entire span of the center section.
?
CONFIDENTIAL
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Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
11-12
CONFIDENTIAL
11-12
Mfr.
Type
Designer: Ii ?. n
Light Transport
Crew
5
PERFORMANCE
July
1953
Maximum Speeds; 225 knots o S.L.; 218 knots it 15'060 ft alt.; knots e ft alt.
Cruising Speeds: Normil power 220 knots 0 10000 ft ail.; Economical1122knots 10000 ft alt.
Climb: 11.7 mins. to 15000 ft alt.; Rate of Climb: 1400 ft/min. it SL ft alt.
Service Ceilings: 25500 ft with normal weight; 25500 ft with 35500 lbs weight
Take-Off distance over 50 ft obstacle' 1890 ft Into zero wind at Sea Level
Fuel: (US gals.) Internal: Normal , Maximum 1080 ; External: Normal , Maximum
RANGES
1335
nautical
miles
nautical
miles
nautical
miles
it
162 knots,
10000 ft
alt.
fuel
0
with
knots,
ft
alt.
fuel
0
knots,
ft
alt.
fuel
with
1080
US gals, of
US gals. of
with
US gals. of
and
7500 lbs
cargo
and
lbs
and
lbs
Combat Radius: 665 Nautical Miles
POWER PLANT
No. Engines 2 Take-Off 1825 hp. e SL ft alt.
Normal 6 a hp. 0 5100 ft alt.
Type Eng1nesNeciprocating Military hp. 0 ft alt.
War Emergency hp. 0 ft alt.
Description ASh-82 FN- 1214-cyl nder, ;ir-eonled radial engine
SPECIFICATIONS
2500 rpm 48 in. Ng.
2400 rpm 39 In. Hg.
rpm in. Ng.
rpm in. H5.
SUPERCHARGER PROPELLER
FUEL
Bore_ 6 1 ins Dry Wt. 1980 No. Speeds 2 Mfr. Type 95/115,95/130
Stroke 6.1 _ins Red.Gear .5825 No. Stages 1 No.Blades 4 Grades
Disnl.jWILcu. ins Eng.Width 49.5 in Ratios 7.14:1, 10:1 Dia. 14 ft, 7 Ins
Comp. Ratio Eng.Langth 79 in Impeller Dia 11.4Ina Pitch Control Constant speed, full feather-
ARMAMENT
BOMB/FREIGHT LOAD
Guns
None
GunsIght None
Normal Load
Maximum Load
7500
lbs
Ibs
Passenger capacity redUced to 18
Bombsight None
Armor
lug
COMBAT PROTECTION
None
Fuel Tanks None
SPECIFICATIONS_
Materials All metal construction
Span:32:f_ft,_Lin; Length:_a52__it, 101n; meight:_21__ft,__Lin; Gross Wing Area 1160 sq. ft
Weights: Airframe lbs; Normal Gross Unknown lbs: Maximum Gross 35500 lbs
ADDITIONAL DATA
The 11-12 was first displayed in 1946 as a passenger transport, becoming operational in 1947. It
has since been observed in increasing nuMhers both in Russia and the satellite countries, and is being
built apparently to replace the widely-used Li-2. De-icing of the wings is accomplished by means of
hot-air ducting through the leading edges, utilizing heat exchangers operating from the engine exhaust
gases. The exhaust stacks are ducted to the nacelle-leading edge junction on the outboard sides of the
nacelles. Tail surfaces are also thermally de-iced by auxiliary heating.
In 1950, all civil 11-12 transports were structurally modified due to wing failures. Subsequently
the maximum gross weight was reduced from 38000 lbs to 35500 lbs, and passenger capacity limited to
T4r. A her the military version wait affected similarly; however, such is probable.
CONFIDENTIAL
Aci*
50X1-HUM-
r?ei
March
1952
ALTITUDE -FT
3249110.
20 000
15,000
10 000
5.000
tvt loorrimum
CONFIDENTIAL
SPEED 8 OL/iff8
MINA 1111111 IIIII II
nen111111111111111111 11111misH111111111111
11 1 111131 INHo
111111 1111111111,1111 1111
IL-l2
VEIN wM IIIIIMIIIIIIIIVISIMIMIIMILA1111111^1111111111111111111111MM11.11111MINII
111111111111111W IHHIIHIIIIH
gnu:1
kla111111111111MMIIIMIIIIIIMMIIIMII
MIMIIIIIIMEN MUM
1111111111111111
.111111111111211WAIIII
,1menamskorAminnu
11111111111MIMIIM 1416111111?11111
Time to climb
Max. speed
111111111111111
ampittuinnuntim
1111111M 1111M11111111111111111111111111111111MINIIIIIININZ
111111111111111?1?11111M111111111MIIIIIIIIMIIIIIIMIMI
MUM IIIIIMMIIIIM1111111111W
MIME
Rate of climb
11111M111111 1111111?11111111MIEMI
SPEED?KNOTS 0
5
100
10
1
200
15
1
300
20
25
1
400
1
.500
MIN TO CLIMB 1
0
1 1 1 1 1
10 20 30 40 50
L_Eagmamma1
600
I .
60
DESCRIPTION
Normal rated power,maximmngross weight.
NOTE: Above 5000 ft, maximum power is BHP.
CONFIDENTIAL
50X1-HUM
leffammittrilira:F.T11..
nitize
? ?
rove or e ease
O. I
?A 55 888 8
88
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
IL-12
TAKE-OFF DISTANCE OVER 50 FT. OBSTACLE-FT
CONFIDENTIAL
R
March
3000
2500
TAKE - OFF
---GONGRETE RUNWAY
?
weimmA EMNIIIMEMO ?NEN ???MOIMIM MEN MERM WM EMI
=SRAI t t.m
IBM REM MIIISMMEMEMINIIMM MEM
--- TURF RUNWAY
1952
hIii
ot t
MEM MIIIREMMEAMME MAMMINEM MINIMMEMM
"11
EMU MIMI
II
?i
111161=1111111111111MMENIMMINK6661 MMIUMMIlltalln -41-111111MINNIK11111111111 MEM
I
6 t
tilt it 1 .. 1 it
MUM SUREMMEMEMEREMMIIMMEMMEME USE pmawmAmmmmiewAmmam, x
1 1
I i !
lilt
II : II!' l'i
I ,
ILI: 1111 II II I I1
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, i'1; III 1
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III: im i : . I' 1 II ,
I II ' li
i II , , 1111 1111
ii
HI! 1111 1 I I
1500
GROSS WT-1000LBS
32 34 36 38 40 42 44
L_PEREQEMAHCE_1
DESCRIPTION
?CONFIDENTIAL
50X1-HUM
October
1957
CONFIDENTIAL
CRATE
44!,711=;:5
3
Ii
REMARKS: CRATE is a twin, reciprocating-engine, low-wing, monoplane transport developed from
COACH. It is a product of the Ilyushin design bureau and is designated 11-14.
SUMMARY
Oct 1953 First reported sighting of "blunt-tailed modification" of COACH.
1954 CRATE introduced into service on Soviet airline Aeroflot.
1956 CRATE production initiated in East Germany as 11-141' and in Czechoslovakia as Avia-14.
1956 11-14M, with improved systems and increased seating capacity, introduced in last half.
50X1-HUM
CONFIDENTIAL
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Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
CONFIDENTIAL
CRATE
October
1957
DIMENSIONS
Wing
Span
Area
Root thickness (%)
Tip thickness (%)
Fuselage
Length
Max diameter
Height, tail above
ground
Horizontal tail span
Cargo cabin
Length
Max height
Useable volume
Floor area
104 ft
1075 sq ft
18
12
69.9 ft
9.2 ft
25.6 ft
30.4 ft
33.0
6.36
1500
290
ft
ft
Cu ft
sq ft
POWER PLANT
Nr. & Model
Designer
Type
Cylinders
Displacement
Compression ratio
Length
Diameter
Weight (dry)
Fuel Metering
Supercharger
Propeller
Diameter
Weight
2 x ASh-82T
Ivchenko
Reciprocating,
aircooled radial
14 - double row
2215 cu in.
6.9:1
79.53 in.
51.38 in.
2244 lb
Direct injection
Single stage/
single speed
AV-50
12.5 ft
450 lb
Reduction gear ratio 31:54
WEIGHTS
Loading
Passenger
Cargo
Take-off
36,300
36,300
Empty
26,600
214,600
Payload
2,600
4,600
ENGINE RATINGS
Take-off
Normal rated
BHP
1875
1610
RPM MP
2600 49 in Hg
2400 40 in Hg
SFC .626 - .690
GENERAL INFORMATION
CRATE was developed to correct structural and performance deficiencies in COACH.
Outwardly the differences in appearance are minor, and are confined mainly to the
wings, engines and nacelles, landing gear and vertical tail surfaces.
The fuselage of the I1-1414 is 3.28 feet longer than the 11-14 because of the
addition of .a section ahead of the wing. This section increases the cargo cabin
length' to 36.3 feet, the useable volume to 1650 cubic feet and the floor area to
310 square feet. Also several equipment systems, for example, hydraulic and fire
extinguishing systems, have been improved. AS a result of the changes the take-
off weight, empty weight and payload have all been increased. For the 11-1414
passenger version these weights are .38,000; 27,500; and 3,400 pounds respectively,
and they are 38,500, 25,250 and 5,650 pounds for the cargo variant. The number of
passenger. seats bas been raised from 18 to 24. The 11-14 and 11-1414 power plants
are identical.. 11-1414 is the first significant modification of the 11-14 design.
Performance, data included in these sheets has been based on information in a
Soviet publication for the 11-14. Range and radius performance of the I1-1414 do
not differ significantly from the 11-14; however, take-off run and distance iill
be slightly increased and rate of climb and service ceiling will be slightly
decreased. Exact values are 'presently not available.
Although CRATE is the leading transport on Aeroflot, the Soviet airline, and is
also used by the Soviet Air Force to transport both passengers and cargo, its
flight characteristics are reportedly only fair. The aircraft is very uneconomi-
cal by U.S. standards and falls into a class of U.S. aircraft which fly farther,
faster, and with a greater payload.
FUEL
Fuel Oil
Capacity (US gal)
925 75
Weight (lb)
5500 550
Grade
95/130 Octane
Note: Capacity of fuel identical in
11-14 and 11-144. All fuel
in wing tanks.
PASSJFREIGHT
Pasaengers 18
Cargo (lb) 4600
ELECTRONICS
RADAR
IFF
NAVIGATION
Radio Compass (2)
Radio Altimeter with low altitude
warning system
Localizer Receiver
Glide Path Receiver
Distance Measuring Equipment
COMMUNICATION
VHF Command Set (2)
Liaison Transmitter (2)
Liaison Receiver (2)
Intercom
CREW
Pilot
Co-Pilot
Navigator
Radio Operator
Cabin Attendant (passenger variant)
50X1 -HUM
CONFIDENTIAL
CONFIDENTIAL
October
1957
CRATE
AIRCRAFT PERFORMANCE
ECONOMICAL CRUISE
MAXIMUM
CARGO
LONG
RANGE
CONDITIONS
@ 5,000 ft
@ 10,000 ft
@ 15,000 ft
TAKE-OFF WEIGHT (lb)
36,300
5,500
4,600
33.8
60
1:550
2,700
1,050
5
NA
24,000
36,300
5,500
4,600
33.8
60
1,550
2,700
1,050
5
10
24,000
36,300
5,500
4,600
33.8
60
1,550
2,700
1,050
5
10
24,000
36,300
1,600
8,500
33.8
60
1,550
2,700
1,050
NA
NA
24,000
36,300
5,500
4,600
33.8
60
1,550
2,700
1,050
5
10
24,000
Fuel weight (lb)
Payload (Cargo) (lb)
Wing loading (lb/sq ft)
Stall speed (kn)
Take-off ground run at SL (ft) (1)
Take-off to clear 50 ft (ft) (1)
Rate of climb at SL (ft/min) (2)
Time: SL to 5,000 ft (min) (2)
Time: SL to 10,000 ft (min) (2)
Service ceiling (ft) (2)
COMBAT RANGE (Nm)
1,275
1,400
1,335
320
1,560
Average speed (km)
165
165
165
165
140
Cruise altitude (coast) (ft)
5,000
10,000
15,000
SL
10,000
Mission time (hr)
7.8
8.7
8.4
1.9
11.3
COMBAT RADIUS (Nm)
600
640
600
135
710
Average speed (kn)
165
165
165
165
140
Cruise altitude (const) (ft)
5,000
10,000
15,000
SL
10,000
Mission time (hr)
7.b
8.2
7.6
1.6
10.5
FIRST LANDING WEIGHT (lb)
33,800
33,800
33,800
35,500
33,800
?
,
,
NOTES
(1) Maximum Power 50X1 -HUM
(2) Normal Power
Performance obtained from 11-14 handbook. 11-1414 range-radius not significantly different, take-off run and
distance increased, rate of climb decreased. Values presently not available for 11-144.
CONFIDENTIAL
n
ified in Part Sanitized Copy Approved for Release 2013/08/01 ? CIA-RDP81-01043R002000100005-9
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
3
?
CONFIDENTIAL
November
1957
CAMEL
REMARKS: CAMEL/Tu-104 is a swept-wing monoplane powered by two large axial flow, turbojet
engines. It is similar in appearance to BADGER/Tu-16. Both designs are attributed to A. N. Ttpolev.
CAMEL is in service in two variants: 50 passenger first class and 70 passenger tourist.
Jul 1955
Mar 1956
Apr 1956
Sep 1956
Sep 1957
SUMMARY
CAMEL first observed on Soviet Aviation Day at Moscov/Tushino.
CAMEL arrives at London Airport, London, England.
Three CAMELS land at London Airport.
CAMEL in service on Aeroflot, USSR civil airline.
CAMEL makes two round trips from* Moscow to U.S.
50X1 -HUM
CONFIDENTIAL
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Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 CIA-RDP81-01043R002000100005-9
CONFIDENTIAL
CAMEL
November
1957
DIMENSIONS
Wing
Span
Area
Inboard Sweep (LE)
Outboard Sweep (LE)
Fuselage
Length
Diameter (max)
Height
Tail above ground
Cabin
Length
Height (max)
'Width (max)
Useable volume
114 ft
1990 sq ft
41 deg
36 deg
124 ft
11.5 ft
37.5 ft
85
8
11
5900
ft
ft
ft
cu ft
POWER PLANT
Nr. & Model
Designer
Type
Compressor
Turbine
Pressure ratio
Diameter
Weight (dry)
Gas turbine starter
2 - AM 3
A. Mikulin
Axial flow
8-stage
2-stage
6:1
53 in.
5500 lb
WEIGHTS
Loading
50-Pas8enger Cargo
Take-off
152,500
152,500
Empty
73,200
67,700
Payload
17,500
23,200
ENGINE RATINGS
SL STATIC
LB RPM
Mil 19,000 4700
SPC/.94#/ithrust/hr
Normal
Cruise
17,500 4350
11,000 4000
GENERAL INFORMATION
CAMEL/Tu-104 is a low, swept-wing, twin-engined, high performance aircraft. De-
veloped from BADGER/Tu-16 medium bomber, CAMEL was designed primarily as a civil
passenger airliner. First-class configuration has one six-beat compartment, two
eight-seat compartments, and a 28-seat main passenger cabin. Also provided are
a galley, men's and women's lounges and lavatories.
It is estimated that empty weight of cargo variant would be reduced 5500 pounds
by removal of interior furnishings.
The 70-passenger tourist variant, the Tu-104A, was introduced in July 1957 and
is now on service on Aeroflot. Passenger seats are arranged in two cabins, one
with four rows of four abreast and the other with one row of four abreast and ten
rows of five abreast. Preliminary analysis indicates that the weights have been
increased as follows:
70-passenger
Cargo
Take-off
157,000
157,000
Empty
73,200
67,700 -
Payload
22,000
27,500
It is estimated that the fuel capacity of the Tu-104A is no greater than the
Tu-104, however, the fuel tankage has been rearranged. The Tu-104A has three
tanks in each wing, but the tail tank has been eliminated. The exact arrangement
of the fuselage, wing-center-section tank is unknown.
In addition to the equipment listed to the right, the following items of non-
radiating navigation equipment are installed in CA/EL '
Automatic Dead Reckoning Navigation Indicator
Automatic Astro Compass
High Precision Remote Indicating Directional Gyro
FUEL
Weight 59,000 lb
Two tanks in each wing
Two tanks in fuselage (One in center
section of wing, one near tail)
PASS./FREIGHT
VARIANT
let class
Cargo
50 passengers
23,200 lb
ELECTRONICS
RADAR
Search and Navigation (X-hand)
IFF
NAVIGATION
Radio Compass (2)
DME (distance measuring equipment)
Radio Altimeter (low altitude)
Localizer Receiver
Glide Path Receiver
Navigation Receiver/Indicator
LORAN (low frequency)
COMMUNICATION
VHF Command Radio (2) (4-channel ea)
Liaison Transmitter (5) Receiver (2)
Intercom
CREW
Pilot
Co-Pilot
Navigator
Radio Operator
Flight Mechanic 50X1 -HUM
Cabin Attendant (occasionally two)
CONFIDENTIAL
a ace!
Sanitized Coiv APP
?
CONFIDENTIAL
April
1957
CAMEL
AIRCRAFT PERFORMANCE
CONDITIONS
Basic
Mission (3)
Constant
Altitude
Mission (4)
TAXI-OFF WRIGHT
(lb)
150,000
150,C00
Fuel at 6.7 lb/gal
(lb)
54,000
54,000
Payload
(lb)
16,500
16,500
Wing loading
(1b/sq ft)
15
75
Stall speed (power off)
(kis)
120
120
Take-off ground run at SL
(ft)
3,300
3,300
Take-off to clear 50 ft
(ft)
5,200
5,200
Rate of climb at SL
(fpm) (1)
5,350
5,350
Time: SL to 20,000 ft
(min)
(1) 5.7
(2) 9.3
Service ceiling (100 fpm)
(ft) (2)
37,000
37,000
Time: SL to 30,000 ft
(min)
(1) 11.8
(2) 16.9
COMBAT RANGE
(ie)
2,050
1,400
Average speed
(kts)
460
430
Initial cruising altitude
(ft)
37,700
32,800
Final cruising altitude
(ft)
43,300
32.800
Total mission time
(hr)
4.50
3.40
COMBAT RADIUS
(N()
900
---
Average speed
(kts)
460
__-
Initial cruising altitude
(ft)
37,700
-.-
Final cruising altitude
(ft)
46,300
---
Total mission time
(hr)
3.95
FIRST LANDING WEIGNX
(lb)
123,500
_--
COMBAT MONT
(lb)
104,000
...
Ccabat altitude
(rt) (2)
,
43,200
Combat speed
(kts) (1)
465
-.-
Combat climb
(fial) (1)
375
Combat ceiling (500 fpm)
,
(ft) (1)
42,200
Service ceiling (100'fpm)
(ft) (2)
43,600
__-
Take-off ground run at SL
(ft) (1)
1,500
Take-off ta clear 50 ft .
(ft) (1)
2,700
---
Rate of climb at SL
(flAg) (1)
7,950
---
Max speed at SL
(kts) (1)
580
---
Basic speed at 25,000 ft
(kts) (1)
525
---
IANDING WEIGHT
(lb)
86,500
---
NOTES (1) Maximum power
(2) Normal power
(3) In accordance with Mil-C-5011A specification
(4) Constant-Altitude Cruise Mission normally flown by Soviets
d for Release2013/08/01 ? CIA-RDP81-01043R002000100005-9
CONFIDENTIAL
50X1 -HUM
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
_
?
CONFIDENTIAL
CAYZI,
April
1557
TAKE?OFF
DISTANCE
(1000 FT)
? CLEAR SOFT
GROUND ROLL
0
90 100 120
CLIMB
ALTITUDE
( 1000 FT)
= ?
t7-1FA
60 ""=----
50
40
30
20
10
:14
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140 150 160 180 1 2 3 4 5 6 7 8
GROSS WEIGHT (LB X1000)
RATE OF CLIMB( FT/ MIN XI000)
ALTITUDE
(1000 FT)
60
50
SPEED
MACH LIMIT
40
?
0 1"-,4*.t..'
30
EiESTIMATED
STRUCTURAL
N910====EMEEP=E--
20 aLIM T, 400 KR IAS
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460
500 540 580
VELOCITY-KNOTS
PAYLOAD
( LB X1000)
70
60
50
40
30
20
10
LOAD DISTANCE
Ira
t..4
I
rriI
1U
Iff:?2
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illitiitt
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=
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TAKE-OFF WEIGHT
-I50,000
LB
--.
--,-.
FUEL CAPACITY?
54,000
LB
PASSENGER PAYLOAD=
16,500
LB
---CARGO
PAYLOAD-
23,000
LB
SPACE
L MI
TEDqiiertI ittl
it i
1
lib
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PAYLOAD
74,000
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1000
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4000
NOTE: TAKE-OFF WEIGHT.- NRP 0 COMBAT WEIGHT - NRP
^^""T ''''3HT MAX ?PWR
reu,sew
CONFIDENTIAL
50X1 -HUM
^
CONFIDENTIAL
September
1957
CAMP
REMARKS:
CAMP is a high-wing, twin-turboprop, assault-type transport that is very similar in
appearance to the USAF C-123. Oleg K. Antonov is credited with the design. He reportedly stated that
"my design bureau designation for this type is AN-8 although the military designation will be AN-14 when
this type enters production for the Air Force." Neither of these designations, however, have been
confirmed.
SUMMARY
CAMP was first observed when it was flown for the Soviet Aviation Day celebration at
Tushino in June 1956. CAMP has been seen on several other occasions at the civil airfield in Kiev from
August 1956 through May l957, but only one CAN' airplane has been seen at these times and it has always
been parked in approximately the same location. It is probable that CAMP was built in Kiev because
Antonovls Design Bureau is located in that city and a CAMP fuselage has been observed outside a Kiev
factory. Moscow press statements that CAMP was not satisfactory appear to have referred to a consider-
ation of passenger operation by the Soviet civil airline (Aeroflot) and do not necessarily reflect on
its acceptance for freight or military purposes.
50X1 -HUM
CONFIDENTIAL
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
CONFIDENTIAL
CAMP
September
1957
DIMENSIONS
Wing
Span
Area
Aspect Ratio
Fuselage
Length
Maximum Width
Maximum Depth
Usable Cabin
- 125 ft.
- 1310 sq. ft.
- 11.9
- 103 ft.
- 10.5 ft.
- 12.5 ft.
- 2900 Cu. ft.
POWER PLANT
Engine Type
Nc. of Engines
Model
Propeller:
Diameter
No. Blades
Turboprop
2
Unknown
16 ft
4
Type: Single-Rotation, Hylromatic,
and Featherable.
WEIGHTS
Empty
1,1,000
Crew (5)
1,000
Fuel
16,000
Payload
17,000
Normal Gross
75,000 lb
ENGINE RATINGS
MILITARY POWER
Altitude Speed SHP Net Prop
Thrust Elf
S L Static 3630 1000 lb 74.7
NORMAL RATED POWER
Altitude
Speed
SHP
Net
Prop
Thrust
Eff
S L
150kn
3280
520 lb
83.7
S L
300kn
3640
220
83.7
S L
350kn
3800
130
79.6
10,000 ft 350kn
3250
150
79.6
20,000 ft 350kn
2570
155
73.1
GENERAL INFORMATION
subsequent to the accomplishment of the above estimates, it was reported
that Antonov had stated that the airplane was "powered by two 5100 hp. engines."
If this figure referred to SHP instead of ESHP it could indicate the A-Model-2
engine (normally 5640 ESHP) which was developed from the German JUM0-022. Itis
possible that, the prototype CAMP was powered by two A-Model-2 engines; photo-
interpretation of the nacelle sizes indicated that sufficient space was avail-
able. It is not, known that 4000 ESHP engines were available at the time of the
1956 7Vshino airshow. However, the preponderance of information indicates that:
The performance with 4000 ESHP engines is adequate for the estimated mission and
reports indicated that at least two different Soviet designs of h000 ESHP turbo-
prop engines are available, which strengthens the estimate that 1,000 ESHP en-
gines will be installed if and when CAMP is placed into production and service.
Large, blister-like fairings on either side of the lower fuselage un-
doubtedly house the main landing gear. It is probable that a multiple-wheeled
arrangement of low-pressure tires is utilized to permit operation into relatively
unprepared fields. The nose gear, probably dual-wheeled, retracts into the
fuselage behind the chin-radome.
An assault-type mission, for the supply or re-supply of men and materiel
in close support of combat areas, is indicated by the general appearance and
especially: The landing gear, high wing, tail turret, and ramp docr. An
analysis of the propeller shown in available photography was made with consider-
ation of the critical take-off requirements of an assault-type mission. This
analysis indicated that the propeller woUld develop optimum efficiencies at
about 250 knots speed and 10,000 ft altitade when utilized with an engine of
about 3500 installed shaft horsepower. Distances shown on the take-off curves
are for concrete-runway operation because of standard comparative purposes; sod
field operation increases the ground run by 5-10 percent, depending on the soil
condition.
Due to the maximum altitudes attainable by the aircraft, the crew com-
partment is probably pressurized in addition to being equipped with oxygen-
breathing equipment. However, it is estimated that the fuselage cabin is not
pressurized, although oxygen-breathing equipment may be installed to enable
troops to maintain physical condition for'post -landing activity.
FUEL
Normal capacity is estimated
at 16,000 lb, which is equivalent
to 2376 U S gallons or 9000 liters.
It is assumed that additional fuel
up to a total 17,000 lb can be
carried in lieu of payload if tem-
porary auxiliary tankage is in-
stalled.
BOMBS/FREIGHT
NORMAL PAYLOAD - 17,000 lb
(May include large, wheeled items
that can be loaded through the
ramp-loading door at the rear of
the usable cabin)
NORMAL TROOP CAPACITY - 60
(Limited by space considerations)
ELECTRONICS
Range-Only Tail Radar
IFF
Radar Warning Rovr
Navig Radar
Radio Cmpassee (2)
ILS System
Hark. Beacon Row
Distance Meas. Equip
Radio Altimeter
Long Range Navig. S'at.
VHF Command Set
Liais. Commun, Transmtr
Liais. Commun. Receiver
Interphone
SRO
APS-54
MUSHROOM
ARK-5
MATERIK
MRP-48P
SD-1
RV-2
MOON
RSIU-3M'
RSB-70
US-9
SFU-10
GUNS
2x23 m.m. (Tail Turret)
Optical computing sight with radar
ranging and manual tracking.
?
t
ROCKETS
None
OX1 -HUM
CONFIDENTIAL
?
CONFIDENTIAL
September
1957
CAMP
AIRCRAFT PERFORMANCE
CONDITIONS
15,000
Ft
20,000
Ft
BASIC
MISSION
FERRY
MISSION
TAKE-OFF WEIGHT (lb)
Fuel at 6.7 lb/gal (lb)
Payload (Cargo) (lb)
Wing Loading (1b/sq ft)
Stall Speed (Power Off) (kn)
Take-Off Ground Run at S L (1) (ft)
Take-Off to Clear 50 Ft (1) (ft)
Rate of Climb at s L (2) (fpm)
Time: S L to 20,000 Ft (2) (min)
Service Ceiling (100 fpm) (2) (ft)
75,000.
16,000
17,000
57.
94
1,950
2,700
1,760
17
30,800
75,000
16,000
17,000
57.
94
1,950
2,700
1,760
17
30,800
75,000
16,000
17,000
57.
94
1,950
2,700
1,760
17
30,800
75,000
31,000
None
57.
94
1,950
- 2,700
1,760
17
30,800
COMBAT RANGE (NM)
1,130
1,235
1,445
3,870
Average Speed (kn)
230
240
230
230
Initial Cruising Altitude (ft)
15,000
20,000
32,000
32,000
Final Cruising Altitude (ft)
15,000
20,000
36,200
43,400
Total Mission Time (hr)
5.0
5.2
6.5
17.5
COMBAT RADIUS (NM)
560
610
735
Average Speed (kn)
225
230
230
Initial Cruising Altitude (ft)
15,000
20,000
32,000
Final Cruising Altitude (ft)
15,000
20,000
42,900
Total Mission Time (hr)
5.1
5.4
6.8
FIRST LANDINC WEIGHT (lb)
67,600
67,500
67,000
COMBAT WEIGHT (lb)
50,600
50,500
50,000
Combat Altitude (ft)
15,000
20,000
40,800
Combat Speed (2) (kn)
280
280
230
Combat Climb (2) (fpm)
1,900
1,600
100
Combat Ceiling (5C0 ppm) (2) (ft)
36,200
36,400
36,600
Service Ceiling (100 fpm) (2) (ft)
40,400
40,500
40;800
Take-Off Ground Run at S L (1) (ft)
1,230
1;220
1,210
.
Take-Off to Clear 50 Ft (1) (ft)
1,900
1,900
1,880
Rate of Climb at S L (2) (fpm)
2,930
2,940
2,980
Maximum Speed at 17,000 Ft (2) (kn)
280
' 280
. 280
Basic Speed at 25,000 Ft (2) (kn)
280
280
280
LANDING WEIGHT (lb)
44,100
414,100
44,100
44,900
-
'
-
NOTES
(1) Military Power
(2) Normal Rated Power
CONFIDENTIAL
INa!
50X1 -HUM
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
CONFIDENTIAL
CONFIDENTIAL
Septeher
1957
October CAT
1957
TAKE-OFF
CLIMB
DISTANCE
(I000FT)
ALTITUDE
(1000 FT)
SEA LEVEL-STANDARD DAY
CONCRETE RUNWAY
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GROUND RUN
RU
0 0 I A
40 50 60 70 80 0 1000 2000 3000
GROSS WEIGHT (1000 LB)
SPEED
RATE OF CLIMB-FT/MIN
ALTITUDE
(1000 FT)
PAYLOAD-RANGE
PAYLOAD FUEL LOAD
(1000LB) (1000 LB)
GW.75,000 LB
PH1 11
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NORMAL POWER
200 220 240 260 280
TRUE AIR SPEED (KNOTS).
0
0 1000 2000 3090 4000
REMARKS: CAT is a high-wing, monoplane transport powered by four turboprop engines which drive
four-bladed propellers. It is a product of the Antonov design bureau. Its designation is unknown, but
it is called "Ukraina" by the Soviets.
50X1-HUM
DISTANCE IN (NAUTICAL MILES)
Sep 1956
Mar 1957
Apr 1957
Jul 1957
SUMMARY
0. K. Antonov states that his design bureau is building a transport powered by four
turboprop engines.
Photographs and some performance data about CAT released in Soviet press.
First sighting of CAT.
First public display of CAT at Moscow/Vnukovo Airfield. .
50X1-HUM
CONFIDENTIAL
CONFIDENTIAL
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
Declassified in Part- Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
CONFIDENTIAL
CAT
October
1957
DIMENSIONS
Wing
Span
Area
Fuselage
Length
Diameter (max)
Height (Vert. tail above
aircraft center line)
Horizontal tail span
Cabin
Length
Height (max)
Width (max)
Useable volume
Floor area
120 ft
1285 sq ft
110 ft
13.5 ft
25.0 ft
38.0 ft
67.0 ft
8.5 ft
12.5 ft
5500 cu ft
650 sq ft
POWER PLANT
Nr. & Model
Designer
Type
Weight
Propeller diameter
4 x NK-4
N. D. Kuznetsov
Axial flow turboprop
2200 lb
14.65 ft
WEIGHTS
FUEL
Passenger
Cargo
Take-off
110,000
110,000
Empty
6o,400
56,1400
Payload
26,200
30,200
Weight 20,500 lb
ENGINE RATINGS
LB
ESHP sap' THRUST ESFC ALT
Take-off 4000 3560 960 .589 SL
Normal 3440 3065 935 .624 SL
PASS/ FREIGHT
Variant
1st class
Tourist
Cargo
84 passengers
126 passengers
30,200 lb
?
Ii
GENERAL INFORMATION
CAT is a high-wing, four turboprop transport designed by the group directed by
O. K. Antonov. It appears to be typical of Antonov designed aircraft. The
sturdy structure and rugged landing gear, and the large amount of power installed,
allow operation from remote, relatively unprepared airfields. Ostensibly CAT has
been designed as a civil passenger transport; however, the large cabin volume and
internal dimensions indicate that it could easily be used to transport cargo.
The Soviets claim that CAT will be produced in two variants; first-class and
tourist. The former is to seat 84 passengers and the latter 126. The first-
class variant was displayed in July 1957 at Moscow/Vnukovo Airfield but the
tourist variant has not been seen.
ELECTRONICS
RADAR
MUSHROOM (X-band)
IFF
COMMUNICATIONS
VHF Command Radio (2) (4 channel)
HF Liaison Radio (2)
Intercom
NAVIGATION
MOON Navigation Receiver
DME
Radio Compass (2)
Localizer
Glide Path
' Marker Beacon
Radio Altimeter (low level)
CREW
Pilot
Co-Pilot
Navigator
Radio Operator
Cabin Attendant (Civil Variant)
50X1-HUM
CONFIDENTIAL
'ft
_
CONFIDENTIAL
October
1957
CA
AIRCRAFT PERFORMANCE
CONDITIONS
Basic Mission
15,000
25,000
FERRY
TAKE-OFF WEIGHT (lb)
110,000
27,700
20,500
110,000
27,700
20,500
110,000
27,700
20,500
82,300
20,500
Payload (lb)
Fuel at 6.7 lb/gal (lb)
Wing loading (lb/8g ft)
85
85
85
64
Stall speed (power off) (kn)
115
115
115
100
Take-off ground run at SL (ft) (1)
2,300
2,300
2,300
1,200
Take-off to clear 50 ft (ft) (1)
3,700
3,700
3,700
2,450
Rate of climb at sea level (rpm) (1)
2,750
2,750
2,750
3,950
Time: SL to 20,000 ft (min) (2)
12
12
12
8
Service ceiling (100 fpm) (ft) (2)
33,400
33,400
33,400
39,900
Time: SL to 30,000 ft (min) (2)
26
26
26
14
COMBAT RANGE (NM)
1,250
goo
1,200
1,800
Average speed (k11)
335
300
300
335
Initial cruising altitude (ft)
31,800
15,000
25,000
38,800
Final cruising altitude (ft)
35,300
15,000
25,000
43,000
Total mission time (hr)
4
3
4
5.5
COMBAT RADIUS (NM)
665
450
570
Average speed (kn)
335
290
\ 285
Initial cruising altitude (ft)
31,800
15,000
25,000
Final cruising altitude (ft)
43,000
15,000
25,000
Total mission time (hr),
4.5
3
?. 4
FIRST LANDING WEIGHT (lb)
99,700
0 100 70
,
100,200
COMBAT WEIGHT (lb)
72,000
_
73,000
72,500
Combat altitude ' (ft)
40,700
15,000
25,000
Combat speed (kn) (1)
375
390
390
Combat climb (rpm) (1)
525
3,100
2,200
Combat ceiling (500 fpm) (ft) (I)
41,100
40,600
40,900
Service ceiling (100 fpm) (ft) (2)
42,600
42,400
42,500
Take-off ground run (ft) (1)
goo
goo
900
.
Take-off distance (ft) (1)
1,800
1,800
1,800
Rate of climb at SL (fP1n) (1)
4,650
4,550
4,600
Max speed at opt alt (kn/ft) (1)
400/28,000
400/28,000
400/28,000
Basic speed at 25,000 ft (kn) (1)
400
400
, 400
LANDING WEIGHT (lb)
64,900
64t900
64,900
64,900
NOTES (1) Military power
(2) Normal power
50X1 -HUM
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 ? CIA-RDP81-01043R002000100005 9
CONFIDENTIAL
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
41)
11)
c'4
July
1953
CONFIDENTIAL
P0-2
REMARKS:
The POLIKARPOV P0-2 is one of the oldest aircraft still in use by the USSR. Its original designa-
tion was U-2 and was redesignated P0-2 in 1944. Although it is primarily a trainer, it is sometimes
employed as a light bomber for night intruder missions. There are pest control, glider tug, photo-
mapping, and adbulance versions of this aircraft. The P0-2 maybe equipped with skis or floats. A ver-
sion of this aircraft has been reported with an in-line engine (probably M-5).
SUMMARY
1953 The P0-2 under the desigdation U-2 was first publically exhibited at the Berlin
Air Show in October 1928. It has been produced in Poland (under designation CSS-13) and
also in Yugoslavia. As late as 1950 it was still in production in the USSR. This air-
craft was used in Korea for night heckler missions.
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CONFIDENTIAL
50X1 -HUM
P0-2
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
CONFIDENTIAL
July
1953
DIMENSIONS
Span 37 ft 5 in
Length 27 ft 2 in
Height 13 ft 0 in
Wing Area 370 sq ft
POWER PLANT
Engine
Type
M-11D
Reciprocating 5-
cylinder, air-
cooled, radial
Diameter 42.3 in
Dry Weight 429 ).ba
(with accessories)
WEIGHTS
Take-off Gross Weight 2660 lbs
ENGINE RATINGS
BHP/RPM
T.O. Power 123/1760
NB? 115/1700
Cruise 101/1640
(All powers at SL)
FUEL
Location
Internal*
Gallons
140
Grade 70 octane
* Mounted in front of forward cock-
pit, gravity feed system. Not pro-
tected.
BOMBS/FREIGHT
Bomb Load
Max Load
4 x 55 lb bombs.
loaded externally
-220 lbs
GENERAL INFORMATION
a. Fixed conventional landing gear with airfoil spreader bar, shock cord struts
adjustable tension by turnbuckle. Controllable tail skid. No brakes in-
stalled.
b. Two blade VD-451 E fixed pitch wooden propeller 7 ft 10 in, in diameter.
c. Open cockpit, two place in tandem with dual controls. Blind flying hood on
rear cockpit. No armor protection.
d. Equipped for night flying.
e. All wood construction - fabric covered.
f. Wings are of unequal span and parallel chord; tips are rounded. Main bracing
is by interplane struts with vire cross bracing.
ELECTRONICS
None
GUNS
2 x 7.62 mm synchronized
2 x 7.62 mm flexible in rear Cockpit
Guns may be omitted.
ROCKETS _
None
CONFIDENTIAL
?
AtlY
1953
CONFIDENTIAL
P0-2
AIRCRAFT PERFORMANCE
CONDITIONS
BASIC
MISSION
TAKE-OFF WEIGHT
(lb)
2660
Fuel at 6.0 lb/gal (grade 70)
(lb)
240
Payload (crew)
(lb)
400
Wing loading
(lb/sq ft)
7.2
Stall speed (power off)
(kn)
40
Take-off-ground run at SL
(1)
(rt)
950
Take-off to clear 50 ft
(1)
(rt)
1150
Rate of climb at SL
(2)
(rpm)
630
Time: SL to 5000 ft
(2)
(min)
11.5
Time: SL to 10000 ft
(2)
(min)
3345
Service ceiling (100 rpm)
(2)
(rt)
12300
COMBAT RANGE
(3)
(10.1)
357
Average cruising speed
(Ito)
66
Cruising altitude
(rt)
5000
Total mission time
(hro)
5.4
COMBAT RADIUS
(3)
(NM)
168
Average cruising speed
(kn)
66
Cruising altitude
(ft)
5000
Total mission time
(bra)
5.1
FIRST LANDING WEIGHT
(4)
(lb)
2550
Ground roll at SL
(ft)
352
Total from 50 ft
(ft)
1290
COMBAT WEIGHT
(4)
(lb)
2550
Combat altitude
(ft)
5000
Combat speed
(1)
(kn)
84
Cat climb
(1)
(fpm)
445
Combat ceiling (500 rpm)
(1)
(ft)
3600
Service ceiling (100 rpm)
(2)
(rt)
12750
Take-off ground run at SL
(1)
(ft)
1025
Take-off to clear 50 ft
(1)
(rt)
1260
Max rate of climb at SL
(1)
(rpm)
675
Max speed at SL
(1)
(kn)
86
Basic speed at 5000 ft
(1)
(kn)
84
SECOND LANDING WEIGHT
(4)
(lb)
2444
Ground roll at SL
(ft)
330
Total from 50 ft
(rt)
1245
-
,
NOTES (1) T.O. Power (Max RPM - 1760)
(2) Normal Power (Normal RPM - 1700)
(3) Range and Radius Mission as per MIL-C-5mA
(4) For Radius Mission
CONFIDENTIAL
41?01?3..moi
50X1 -HUM
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
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Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
CONFIDENTIAL
CONFIDENTIAL
MAX (Yak-18)
Mfr Designer: Yakovlev Crew
Type Trainer
PERFORMANCE
Maximus Speeds. 238 knots e S.L.; 261 knots e 7880 ft alt.; 245 knots a 16400 ft alt.
Cruising Speeds: Normal Power knots V ft alt.; Economical 160 knots e 5000 ft alt.
Climb; 5 Pins. to 10000 ft sit.: Rate of Climb. 2000 ft./min. at SL ft alt.
Seriice Ceilings: 22000 ft with normal weight; ft with lbs weight
Take-Off distance over 50 ft obstacle ft Into zero wind at Sea Level
Fuel; (US gals.) internal: Normal 50 , Maximum 96 ? External: Normal , Maximum
248 nautical miles
e__164knots, 5000 ft alt
with 50 US gals, of fuel
and no lbs bombs
RANGES
450 nautical miles
I 155 knots, 5000 ft alt.
with 96 US gals. of fuel
and no lbs bombs
Combat Radius: 110 Nautical Miles Combat Radius: 200 Nautical Miles
POWER PLANT
nautical miles
? knots, ft alt.
with US gals. of fuel
and lbs
No. Engines 1 Take-Off 690 hp. e SL ft alt. 2100 rpm in. NI.
Normal hp f ft alt. rpm in Hg.
Type Engines BelprocatingMilitary 650 hp. 5575 ft alt. 2800 rpm 33 In. WI.
War Emergency hp. e ft alt. rpm in. Ng.
Description
ASh-21, 7-cylinder, air-cooled radial
SPECIFICATIONS SUPERCHARGER PROPELLER FUEL
Bore 6.1 Ins Dry it No. Speeds 1 Mfr. VISCH-111-B-20 Type Gasoline
Stroke 6.1 ins Red.Gear No. Stages 1 lio.Blades 2 87 octane
Dispi. cu. ins Eng.Width 49.5 in Ratios 7:1 Dia. ft, ins
Comp. Ratio_._ Eng.Length 54 in Impeller Dia ins Pitch Control
ARMAMENT
BOMB/FREIGHT LOAD
COMBAT PROTECTION
Guns
Normal Load None lbs
Armor
None
1x12.7 mm/100 rp m, synchronized.
220
Load lbs
.
,maximum
Stowage: Under wing.
_BEREZINA
2x110 lb bodhs
Guneight
PBP VA Reflector type
Bombsight None
Fuel
Tanks
None
SPECIFICATIONS
REMARKS: . The Yak-18 is one of the latest Soviet piston engine trainers. It is an improved
version of the Ut-2. A tricycle version, designated Yak-18U, and revealed during 1956, is reportedly
slightly heavier.
Materials Mixed wood and metal construction
Span*.11._ft,J&In; Length. 27 ft,Ja_in; Height; 10 ft,_IL_In; Gross Wing Area 176 - sq. ft
Weights; Airframe 1530 lbs; Normal Gross 47015 lbs; Maximum Gross 5313 lbs
ADDITIONAL DATA
50X1 -HUM
SUMMARY
1947 First observed and presumed to be in service.
1951 Aircraft widely used, such as by the Soviet Aero Clubs in competitive sports events and airshows.
1954 Established FAI records (2200-3850 lb weight class): Closed-course distance of 1245 NM,
Altitude of 20,705 ft.
1956 Formations of from 24 to 94 perform at Aviation Day Airshows since 1949.
The Yak-11 aircraft is about the same size as the U.S. AT-6, and is somewhat similar in appear-
ance with the long greenhouse. It is a relatively new trainer and believed to have been placed in
use in 1947. It was thought at one time that the Yak-11 was a fighter type aircraft instead of a
trainer.
50X1 -HUM
CONFIDENTIAL
CONFIDENTIAL
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
CONFIDENTIAL
MAX (Yak-18)
July
DIMENSIONS
Wing
Span
Area
Dihedral
Length
Height
34 ft 9 in
183 sq ft
7'
26 ft 4 in
10 ft 4 in
Height (3 point attitude) 6 ft 11 in
Landing gear tread 6 ft 10 in
POWER PLANT
Engine M-11-FR-1
Bore 5.9 in
Stroke 6.1 in
Type Reciprocating,
5-cylinder, air-
cooled, radial
Diameter 42.5 in
Length 37.2 in
Dry Weight 429 lb
(with accessories)
WEIGHTS
Take off gross weight 2400 lb
ENGINE RATINGS
Take-off
Normal rated power
Cruise (75% ERP)
(Al). ratings at SL)
BHP/RPM
158/1900
140/1760
105/1600
GENERAL INFORMATION
a. Conventional landing gear with retractable main wheels. Main struts
project into airstream when retracted. Full swiveling tail wheel is
fixed.
b. Two blade V-510-D-81 propeller, 6 ft 6 1/2 in diameter.
c. Basic structure metal throughout, wing, empennage and aft section of
fuselage fabric covered, remainder covered with metal.
d. Two sesta in tandem. Sections of plexiglass canopy slide back for
access to cockpits.
e. Equipped for night flying. 24V battery.
f. Landing gear and flaps are pneumatirally operated.
g. A version with tricycle landing gear has been observed.
h. Variations in aircraft performance between the calculated and the
flight test on following page results from different propellers
being utilized.
FUEL
Location
Internal*
Grade
Oil
44 gal
tO Octane
4 gal
*Two (2) tanks in wing center
section; capacity, 22 gal each
BOMBS/FREIGHT
2 x 110 lb
One 110 lb bomb on each of tvo
external racks mounted on underside
of wing center section.
ELECTRONICS
Transmitter
Receiver
Radio Compass
RSI-6K
RSI-6M-1
PCN-6K-NO
GUNS
None
50X1 -HUM
ROCKETS
None
CONFIDENTIAL
CONFIDENTIAL
July
1956
MAX (Yak-1S)
AIRCRAFT
PERFORMANCE
CONDITIONS
Calculated
Basic
Mission
USAF
Flight Test
TAKE-OFF WEIGHT
(lbs)
2500
2500
Fuel (43.5 gal)
(lba)
252
252
Payload (crew)
(lbs)
390
390
Wing Loading
(Na)
13.8
13.8
Stall Speed
(kts)
(2)
46
47
Tb O Ground Run
(ft)
(2)
3.3.30
690
Wo to clear 50 ft
(ft)
(2)
1420
1330
Rate of Climb at S.L.
(fpm)
(2)
700
800
Time to Climb - SL to 5000 ft
(tin)
(2)
9
9
Time to Climb - SL to 10000 ft
(min)
(2)
25
24
Service Ceiling
(ft)
(2)
11500
12000
COMBAT RANGE
(ma)
(5)
420
_-
Average Cruising Speed
(kts)
97
--
Cruise Altitude
(ft)
5000
--
Total Mission Time
(bra)
4.5
--
COMBAT RADIUS
(on)
(5)
196
--
Average Cruising Speed
(kts)
97
--
Cruise Altitude
(ft)
5000
--
Total Mission Time
(bra)
4.2
--
FIRST LANDING WEIGHT
(lbs)
(4)
2400
--
Ground Roll
(ft)
650
--
Total From 50 ft
(ft)
1200
--
COMBAT WEIGIfr
(lbs)
(4)
2400
2400
Combat Altitude
(ft)
5000
5000
Combat Speed
(kts)
116
126
Combat Rate-of-Climb
(fIxn)
450
610
Combat Ceiling (500 fcm)
(ft)
4000
7500
Service Ceiling (100 fpm)
(ft)
13000
13500
T/O Ground Run
(ft)
1040
590
Wo to Clear 50 ft
(ft)
1300
1200
Maximum Speed at S.L.
(kts)
(3)
118
127
Basic Speed at 5000 ft
(kts)
115
122
SECOND LANDING WEIGHT
(lbs)
(4)
2320
--
Ground Roll
(ft)
610
--
Total From 50 ft
(ft)
1150--
?
NOTES
(1) Max Attainable Power - 1950 rpm at S.L. and 1760 at 11,000 ft - Flight Test Aircraft
(2) Clean Configuration
(3) Normal Power - 1760 rpm
(4) For Radius Mission
(5) Range and Radius per MilC 5011A
CONFIDENTIAL
50X1 -HUM
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 ? CIA-RDP81-01043R002000100005-9
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
MAX (Yak-18)
DISTANCE
(1000 FT)
CONFIDENTIAL
TAKE-OFF
SEA LEVEL
ALTITUDE
(1000 Fl)
18 :3: , LI
? 0..
16=-1
, ? Er-
,- OVER 50 FT -
OBSTACLE -
=
July
1956
SPEED
r
- CALCULATED
? FLIGHT TESTS
?4
-
CALCULATED
? FLIGHT TESTS
Th ROUND ROLL?
'
????
-"--JggEt
????--
2.1 22 23 2.4 2.5
VELOCITY
KNOTS
GROSS WEIGHT (1000 lb)
t:
o
60 80 100 120
KNOTS
140
TURN RADIUS
--- CALCULATED
?FUGHT TESTS RS
25? LB T.O. GW
5000 FT CRUISE ALT. -Z.?
LAND AT REMOTE BASE
120----
-17-EE1-7-E-E'
110
100
90
14,0 160 180 200
NAUTICAL MILES
1
r i
?
1=2-
= COMPUTED
--???
?
717.1
=1.
maw;
220
10 20 30 40 50 60
TIME T,0 CLIMB - MIN
200 400 600 800 1000 1200
RATE OF CLIMB - FT/ MIN
:150X1-IUM
CONFIDENTIAL
?
?
July
1953
S S R
CONFIDENTIAL
UIL -28
UI1-28
1
DESCRIPTION
This aircraft is a trainer version of the 11-28. The main differences being the solid
nose section and the twin cockpit.
CONFIDENTIAL
50X1 -HUM
_X\
Declassified in Part - Sanitized Copy Approved for Release 2013/08/01 : CIA-RDP81-01043R002000100005-9
1VIIN301JN03
6-900001-000Z001?1701-0-1-8dC11-V10 1-0/80/?1,0Z 3seeiei ..104 panaddv Ado Pez!4!ueS u! Peq!sseloeCI
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