SOVIET TECHNICAL MANUALS FOR THE R11F-300 TURBOJET ENGINE
Document Type:
Collection:
Document Number (FOIA) /ESDN (CREST):
CIA-RDP80T00246A071200240001-4
Release Decision:
RIPPUB
Original Classification:
S
Document Page Count:
185
Document Creation Date:
December 27, 2016
Document Release Date:
October 28, 2013
Sequence Number:
1
Case Number:
Publication Date:
January 1, 1964
Content Type:
REPORT
File:
Attachment | Size |
---|---|
CIA-RDP80T00246A071200240001-4.pdf | 17.87 MB |
Body:
50x1
Declassified in Part - Sanitized Copy Approved for Release 2013/10/28: CIA-RDP80T00246A071200240001-4
CENTRAL INTELLIGENCE AGENCY
This material contains information affecting the National Defense of the United States within the meaning of the Espionage Laws, Title
18, U.S.C. Secs. 793 and 794, the transmission or revelation of which in any manner to an unauthorized person is prohibited by law.
S-E-C-R-E-T
NO FOREIGN DISSEM
50X1
COUNTRY USSR - REPORT
SUBJECT
DATE OF
INFO.
PLACE &
DATE ACQ.
Soviet Technical Manuals for
the R11F-300 Turbojet Engine
DATE DISTR.
NO. PAGES
REFERENCES
January 1964
50X1-HUM
THIS IS
I INIFVA I I i ATrn INFORMAVIC1N SCIIIRCP ARAIIINIAC ADP IIFFINITIVF APPRAICAI AP CAMTPAIT IC IMITATIVF
5
4
3
2
English- 50X1-HUM
language manuals. classified SECRET by the Sovietsl
No publishing data...were given.
a. RlIF-300 Engine, Operating Instructions, 200 50X1,-HUM
anZ two insets. The text is prefaced with a comment
that the drawings specially supplemented to the book
are deAignated with Roman numerals and those contained
in the rAlbum of Drawings are designated with Arabic
numerals. Unfortunately, the Album of Drawings is
not available.
b. R11F-300 Engine, Technical Description, 142 pages.
' 50X14-IUN
The figures mentioned in the text are not included and
probably are found in the Album of Drawings.
Comment: The R11F-300 engine is installed..::
in MI6-21 (F:SHBED) aircraft. Ten Soviet technical manu
on the MIG-21F-13 aircraft were published previously
th.en-"mantfals refer ta the50x1 -HUM
50X1-HUM
engine as 37F.
Distribution of Attachments:
ORR: 2 copies
OSI: 2 copies
CIA Markings Center:
Air: 5 copies
Air/FTD:6 copies
'SAC: 1 copy
Navy: 2 copies
Navy/STIC:1 copy
copy Army: 3 copies
NSA: 2 copies
S-E-C-R-E-T
NO FOREIGN DISSEM
50X1-HUM
50X1-HUM 5'
4
3
2
1
GROUPI
Excluded from
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STATE
IDM I ARMY I NAVY
I AIR
I Km IXAXEX NIC I OCR
Air/FTD, NAVY/STIC
SAC
(Note: Field :distribution indicated by "#".)
50X1-HUM
Declassified in Part - Sanitized Copy Approved for Release 2013/10/28 : CIA-RDP80T00246A071200240001-4
Declassified in Part - Sanitized Copy Approved for Release 2013/10/28: CIA-RDP80T00246A071200240001-4
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/10/28: CIA-RDP80T00246A071200240001-4
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Declassified in Part - Sanitized Copy Approved for Release 2013/10/28 : CIA-RDP80T00246A071200240001-4
_
NO FOREIGN DISSEM
A
R11F-300 ENGINE
Operating Instructions
SECRET
Declassified in Part - Sanitized Copy Approved for Release 2013/10/28: CIA-RDP80T00246A071200240001-4
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Operating Instructions
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PUP-300 ENGINE
Operating Instructions
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C ONTENTS
Engine Operating Principle Page
Main Technical Data
1. General. .10
2. Jet Nozzle Exhaust Area Diameter Values at
Main Engine Ratings 13
3. Engine Control 13
4. Starting System 14
5. Starter-Generator' . ? .15
6. Starting Equipment 15
7. Starting Fuel System .16
8. Starting Flame Igniter Oxygen Supply System . .17
9. Fuel System 19
10. Lubricating System 22
11. Ignition System and Electrical Equipment . . . .24
Chapter I. OPERATIONAL IIMITATIONS
Chapter II. PREPARATION OF ENGINE FOR STARTING PRIOR
TO FLIGHT
1. Filling of Aircraft Main Fuel and Starting Fuel ?
Tanks 33
2. Filling of Engine Oil Tank 34
3. Preflight Inspection of Engine .34 .
C h.ap t er III. CHECKING OF ENGINE ON GROUND PRIOR
TO FLIGHT
?
1. Engine Starting 7. ? ? 36
2. Power Supply Sources ?38
3. Warming-Up and Checking Engine Operation . . .39'
4. Engine Stopping
The Book contains 200 pages and 2 insets.
nprlacsified in Part - Sanitized Copy 'Approved for Release 2013/10/28: CIA-RDP80T00246A0712.0024.0061-4
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ChapterIV. OPERATION OF ENGINE IN FLIGHT Page
1. Engine Operation at Take-Off and during Climbing .44
2. Engine Operation when Accelerating Aircraft at
Augmented Rating 48
3. Flight with Zero or Negative G-Factor 49
4. Engine Operation with Aircraft Going Round . . 49
5. Engine Starting and Stopping in Flight 50
. 6. Trial Flight 51
Chapter V. CARE OF ENGINE
1. General . 52
2. Preflight Engine Inspection 52
3. Postflight Engine Inspection 52
4. Routine Maintenance after First 5 = 1 Hours of
Engine Operation
5. Periodic Maintenance 56
54
6. Routine Maintenance Performed Every 50 = 5 Hours
of Engine Operation .56
7. Routine Maintenance after Expiration of Engine
Service Life 58
Chapter VI. OPERATION OF ENGINE AT SUBZERO TEMPERATURES
1. Preparation of Engine for Operation ? 60
2. Ground Starting, Warning.-Up, Checking, and
Stopping of Engine 61
3. Operation of Engine during Flight 62
4. Keeping Engine Ready for Operation
Chapter VII. ENGINE MOUNTING AND DISMANTLING
Mounting of Engine on Aircraft
I. Engine Transportation
2. Unpacking of New Engine
3. Preparing Engine for Installation on Aircraft .
4. Installation of Engine on Aircraft
5. Last of Aircraft Pipe Lines Connected to Engine .
6. List of Engine Instruments
7. Flushing of Pipe Lines
8. Deprocessing of Engine 71
62
...
64
65
66
67
69
69
9. Engine Cranking
50X1
-5-
Page
73
10. Checking Oxygen System of Main Flame Igniters
and Charging System with Oxygen ? ? ? ? . . . 73
11. First Starting of Engine 74
12. Engine Ground Checking after
13. Engine Stopping
14. Trial Flight
Dismantling of Engine
1. General Information of Engine Processing .
2. Corrosion-Preventive Compounds
3. Internal Processing of Engine
4. Dismantling of Engine from Aircraft
5. External Processing of Engine
First Starting . . ? .75
- ? 75
? ? 76
.? 76
? ? 77
? ? 77
.77
. . 76
6. Packing Engine in Shipping Case .. 78
Chapter VIII. CARE OF ENGINE INSTAMIED ON AIRCRAFT
DURING PARKING PERIODS
Chapter IX. REPLACEMENT OF ENGINE UNITS AND ASSEMBLIES
1. Replacement of Pipe Lines
2. External Inspection of Pipe Lines prior to
Installation
3. Pipe Lines and Fittings Employed for Oxygen
System
4. Installation of Pipe Lines on Engine . . .
5. Units Replaced via Access Holes of Engine
Compartment
Replacement of
Replacement of
Replacement of
Replacement of
Replacement of
Replacement of
Replacement of
Replacement of
Replacement of
Replacement of
Replacement of
Needle
? ? ? ?
rCP-CT-12000BT Starter-Generator
HP-21 0 Fuel Regulating Pump .
HYPT-10 Control Panel . .
4P-3A ti.anlmitter
81
81
82
83
85
.85
86
88
90
90
? 91
BY-4E Control Unit
? ? ?
? ? ?
P-1 Rheostat
40C-1A Feed-Back Transmitter.
91
1IIH-13LIT Fuel Booster Pump . . . ? 92
Non-Return Oxygen Valve 93
HP-221) Pump Regulating Needle . . 93
HP-220 Pump Barostatic Limiter
94
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n,---h-sc?ifinal it, Part - Sanitized Copy Approved for Release 2013/10/28 : CIA-RDP80T00246A071200240001-4 ???.- ? ?'