INPUT REQUIREMENTS OF THE AIRCRAFT INDUSTRY OF THE USSR

• Document Type: CREST
• Collection: General CIA Records
• Document Number (FOIA) /ESDN (CREST): CIA-RDP79R01141A000300080002-7
• Release Decision: RIPPUB
• Original Classification: S
• Document Page Count: 166
• Document Creation Date: December 27, 2016
• Document Release Date: December 12, 2013
• Sequence Number: 2
• Publication Date: June 15, 1954
• Content Type: REPORT

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ECONOMIC INTELLIGENCE REPORT
INPUT REQUIREMENTS OF THE AIRCRAFT
INDUSTRY OF THE USSR
CIA/RR 35
15 June 1954
CENTRAL INTELLIGENCE AGENCY
OFFICE OF RESEARCH AND REPORTS
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EC ONOMIC INTELLIGENCE REPORT
INPUT REQUIREMENTS OF THE AIRCRAFT INDUSTRY OF THE USSR
CIA/RR 35
(CRR Project 33.226)
CENTRAL INTELLIGENCE AGENCY
Office of Research and Reports
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CONTENTS
Summary and Conclusions
Page
1
I.
Introduction
3
A.
Purpose and Scope
3
B.
Description of Inputs
1.
1. Materials
4
2. Labor
5
3. Electrical Energy
5
4. Fuel and Lubricants
5
5. Transportation
6
C.
Method and Scope of Research
6
II.
Materials
7
A.
Materials Technology
7
1. Level of Soviet Aircraft Metallurgy
7
2. Fabrication Techniques
8
B.
Materials Usage
8
1. Major Materials
8
2. Substitute Materials
10
C.
Method of Computing Materials Inputs
?
?
?
*****
12
1. Airframes
12
2. Aircraft Engines
17
D.
Materials Requirements
18
1. Airframes
18
2. Aircraft Engines
23
3. Summary
26
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III.
Labor
A. Characteristics of Soviet Plants
B. Types of Labor Required
Page
26
26
28
1. Skilled
28
2. Direct
30
3. Managerial
32
I. Technical
33
C. Worker Density
33
D. Labor Requirements
35
1. Airframes
35
2. Aircraft Engines
36
3. Summary
37
IV.
Electrical Energy
38
A. Scope
38
B. Method of Estimating Electrical Energy Inputs .
.
?
?
?
38
C. Electrical Energy Requirements
40
V.
Fuel and Lubricants
41
A. Scope
41
B. Method of Determining Coal Input for Heating .
.
.
.
.
41
C. Method of Determining Lubricating Inputs
43
D. Fuel and Lubricants Requirements . . . . .......
44
VI.
Transportation
44
A. Scope
44
B. Method of Estimating Tonnage to Be Transported
?
?
?
44
1. Airframes
44
2. Aircraft Engines
44
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C. Tonnage of Transportation Required
1. Airframes
2. Aircraft Engines
VII. Conclusions
Appendix A. Plant Studies
Appendixes
Page
46
46
46
46
49
Tables
1.
Summary of Requirements of the Soviet Airframe and Aircraft
Engine Industries, 1953 Production and 1956 Capacity ? ?
?
2
2.
Bills of Materials for Soviet Airframes, 1953
16
3.
Materials Input Coefficients for Soviet Airframes, 1953 .
19
4.
Bills of Materials for Soviet Aircraft Engines, 1953 .
20
5.
Materials Input Coefficients for Soviet Aircraft Engines,
1953
20
6.
Gross Materials Requirements for Production of Soviet
Airframes, 1953
21
7.
Gross Materials Requirements of the Soviet Airframe
Industry, 1953 Production and 1954-56 Capacity
23
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Page
8. Gross Materials Requirements for Production of Soviet
Aircraft Engines, 1953 24
9.. Gross Materials Requirements of the Soviet Aircraft Engine
Industry, 1953 Production and 1954-56 Capacity 25
10. Gross Materials Requirements of the Soviet Airframe and
Aircraft Engine Industries, 1953 Production and 1954-56
Capacity ? ? 26
11. Ratio of Direct Labor to Total Labor in US Airframe Branch
Plants during World War II 31
12. Labor Requirements of the Soviet Airframe Industry, 1953
Production and 1956 Capacity 35
13. Labor Requirements of the Soviet Aircraft Engine Industry,
1953 Production and 1956 Capacity 36
14. Labor Requirements of the Soviet Airframe and Aircraft
Engine Industries, 1953 Production and 1956 Capacity .
15. Electrical Energy Requirements of the Soviet Airframe and
Aircraft Engine Industries, 1953 Production and 1954-56
Capacity
? 37
16. Fuel and Lubricants Requirements of the Soviet Airframe
and Aircraft Engine Industries, 1953 Production and
1954-56 Capacity 45
17. Transportation Requirements of the Soviet Airframe Industry,
1953 Production and 1954-56 Capacity 46
18. Transportation Requirements of the Soviet Aircraft Engine
Industry, 1953 Production and 1954-56 Capacity 47
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a
CIA/RR 35 S-E-C-R-E-T
(CRR Project 33.226)
INPUT REQUIREMENTS OF THE AIRCRAFT INDUSTRY OF THE USSR*
Summary and Conclusions
The inputs discussed in this report are confined to the cate-
gories of materials, labor, energy, and services required to
support both current and capacity production of the aircraft in-
dustry of the USSR. The inputs for capQ.city have been projected 3
years in advance of January 1954 and are based upon the assumption that
capacity effort would be initiated on or about 1 January 1954.
The conclusions drawn from this report on the input requirements
of the aircraft industry of the USSR are as follows:
1. The USSR uses less critical materials per pound of airframe
and engine weight than does the US.
2. The Russians will try to conserve critical elements such as
nickel, columbium, cobalt, zinc, molybdenum, and copper in the
* The estimates and conclusions contained in this report represent
the best judgment of the responsible analyst as of 15 ADril 1q54.
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Table 1
Summary Of Requirements- of the Soviet Airframe
and Aircraft Engine Industries
1953 Production and 1956 Capacity
Input
Unit
Amount
1953
Production
1956
Capacity
Material
Ferrous Metals
Metric Tons
73,400
331,000
Nonferrous Metals
Metric Tons
60,300
275,000
Rubber
Metric Tons
1,330
6,240
Glass and Plastics
Metric Tons
589
2,690
Cobalt
Metric Tons
396
1,790
? Labor
Direct
Number of Employees
112,500
262,500
Indirect
Number of Employees
112,500
262,500
Total a/
225,000
525,000
Skilled
Number of Employees
79,000
184,000
Unskilled
Number of Employees
146,000
341,000
Total a/
225,000
525,000
Managerial b/
Number of Employees
45,000
105,000
Technical 137
Number of Employees
41,000
94,000
Energy
Electrical Power
Million Kilowatt-Hours
419
1,310
Coal
Thousand Metric Tons
696
1,280
Services
Transportation c/
Thousand Metric Tons
960
2,480
a. The categories direct and indirect and the categories skilled and
unskilled represent different breakdowns of the same total.
b. For the explanation of these headings, see pp. 32-33.
c. The category of transportation includes all transportation into
both airframe and aircraft engine plants and most of the transportation
out of these plants.
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manufacture of airframes and engines. In conserving these elements,
the Russians will not lower the quality of any material that can exert
a significant bearing on the operational performance of the aircraft.
3. There has been very limited use of magnesium in Soviet air-
craft as compared with equivalent US types.
4. The ratio of steel to aluminum in Soviet aircraft can be
expected to remain high in comparison to US aircraft.
5. The ratios of unskilled to skilled workers and managerial
to production workers are higher in the Soviet aircraft industry
than in the US aircraft industry.
6. The Soviet labor productivity is lower than that of the US;
therefore, the Russians require more labor than the US to produce
a given number of aircraft-in a stated floor area.
7. Soviet aircraft plants have a higher density of workers per
square foot of floor area than US aircraft plants.
I. Introduction.
A. Purpose and Scope.
The purpose of this report is to determine the input re-
quirements of the aircraft industry of the USSR in terms of the cate-
gories of materials, manpower, energy, and services. These inputs
have been consolidated into one report1
in order
to give a more complete coverage of the input requirements of the
industry and in order to make the material more readily accessible
to the users of input information. Only the principal inputs re-
quired for the production of airframe and aircraft engines in the
USSR have been studied. The inputs for associated products such as
components, parts, and guided missiles are not covered in this report.
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B. Description of Inputs.
The inputs considered in this report are materials, labor,
electrical energy, fuels and lubricants, and transportation. Since
many possible subdivisions of these inputs exist, a brief descrip-
tion of the items covered under each of the major categories is
indicated so that the limitations and significance of the figures
can be properly evaluated in terms of over-all significance to the
Soviet economy.
1. Materials.
The materials inputs to the Soviet aircraft industry
discussed in this report are as follows:
a. Ferrous Metals.
(1)
(2)
(3)
Low-Carbon Steel.
Alloy Steel.
Stainless Steel.
b. Nonferrous Metals.
(1) Aluminum.
(2) Copper and Copper Base Alloys.
(3) Magnesium.
(4) Lead.
c. Rubber.
d. Glass and Plastics.
e. Cobalt (Alloying Element).
The list presents a general breakdown of the important mater-
ials utilized in the Soviet aircraft industry. It includes materials
used in airframes, aircraft engines, and landing gear but excludes
wheels, engine accessories, installed electric and electronic equip-
ment, instruments, and similar equipment. The breakdown makes possi-
ble the computation of base metal inputs but does not permit other than
qualitative order-of-magnitude estimates of alloying element inputs.
With the exception of cobalt, the critical alloying elements have not
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been included in this reportsbecause the determination of the exact
amouhts of elements in each material is too complex for exact esti-
mates, the amounts are relatively small, and a wide range of sub-
stitutability of alloying elements is possible. Cobalt has been in-
cluded because it is an extremely critical material and is one of the
few elements used to obtain high-temperature properties.
2. Labor.
The labor inputs are listed in terms of the total labor
required in airframe and aircraft engine plants together with a
breakdown of the requirements by type of labor normally required in
aircraft manufacture. Labor inputs include the categories of total
labor, direct and indirect labor,* skilled and unskilled labor,
managerial employees, and technical employees. The managerial and
technical categories are considered extremely critical to the in-
dustry and to the Soviet economy as a whole. From the information
presently available it is not feasible to attempt labor requirements
analysis in terms of specific skills or positions.
3. Electrical Energy.
The input of electrical energy has also been determined
in terms of total quantity required under present production condi-
tions and under capacity conditions. Electrical energy is presented
in terms of the total kilowatt-hours required per plant.
4. Fuel and Lubricants.
Fuel and lubricants are important inputs to the aircraft
industry in terms of the total demands of the industry upon the
economy as a whole and also as a guide for judging the level of output
in a plant.. In this report, coal is the only fuel considered, as it
* Direct labor refers to those laborers whose work is expended on the
manufacturing process, which includes machining, processing, fabricat-
ing, assembling, installing, testing in the manufacturing area, and re-
work prior to acceptance. Indirect labor refers to all other persohnel
such as the supervisory employees (above the working foreman level) and
their clerical staffs and the employees engaged in inspection, receiv-
ing, storage, shipping, maintenance, janitorial duties, finance,
accounting, and similar duties.
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is the only fuel used for the maintenance of plant facilities. Lubri-
cants considered are oil and grease. The requirements for fuel and
lubricants are based upon analysis of the fuel requirements for each
individual plant. Fuel for testing purposes, however, has not been
Included,
5. Transportation.
Transportation, as a service input, is the most difficult
Input to analyzelsince it is extremely difficult to measure objectively.
It is not feasible to discuss transportation in terms of the normal
measure of ton-miles because of the complexity of determining the
source of every input into the industry. Transportation inputs are
therefore covered in terms of the total tons of transportation re-
quired to support the production of each individual plant and to dis-
tribute the final product to its ultimate destination and through
an analysis of the scope of interindustry shipments of materials,
components, parts, and completed products.
C. Method and Scope of Research.
A complete discussion of the methodology used in estimating
the inputs of the Soviet airframe and aircraft engine industry is
presented in this report. It must be stressed, however, that although
these estimates of input requirements are based upon a complete
analysis of all available information on each plant, the estimates
are subject to several areas of error and must not be considered as
absolute figures.
As a result
of such poor basic information, heavy reliance has been placed upon
determining total input requirements from the total estimated pro-
duction by applying coefficients of inpats required per pound or
other units of measurement of finished product. These coefficients
have been determined from US experience
and are subject to small ranges of error,
whereas the over-all production estimates are subject to an esti-
mated error of plus or minus 30 percent. The estimates have been
presented in this report in terms of the total inputs required by
type of aircraft and by each plant with the same approximate range
of error for both.
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II. Materials.
A. Materials Technology.
The types of materials used in Soviet airframe and aircraft
engine manufacture are basically a function of the technology of the
Soviet aircraft industry. The two factors of Soviet technology which
have the greatest effect upon the type of materials inputs are the
level of Soviet aircraft metallurgy and the fabrication techniques
used in the manufacture of airframes and aircraft engines.
1. Level of Soviet Aircraft 'Metallurgy.
. The level of Soviet aircraft metallurgy is comparable to
that of the US and the UK at the present time. The Russians un-
doubtedly possess very fine metallurgical scientists and research
facilities, and their level of aircraft metallurgy is limited only
by the availability of raw materials. There is every indication that
the Russians are well endowed with basic raw materials with the ex-
ception of certain alloying elements but are somewhat deficient in the
processing and production of the desired materials. To overcome
these-deficiencies the Russians use substitute materials and care-
fully economize in the use of critical materials. The. Russians have
copied many materials from the US, the UK, and Germany in addition
to producing materials to their own specifications. In copying such
materials, the Russians have rarely improved the quality of material
selected for a particular part but have often selected a material of
lower quality. In any part where quality was required, however, they
have consistently demonstrated the ability to provide it. 1/* In
general, the material best suited to their production facilities and
to their labor skill has been selected and quality provided where
quality is required. Sometimes thechoice of materials is clearly
motivated by a requirement to conserve critical alloying elements,
while at other times the choice is motivated by fabrication methods
and labor skills. In addition there is evidence that the availability
of semifinished products such as bar stock, plate, sheets, extrusions,
and tubing is the determining factor in the choice of materials. In
general the use of materials in the Soviet aircraft industry does dif-
fer Considerably from US practice and probably would result in a
slightly smaller requirement for critical materials per pound of
finished product than that of the US.
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2. Fabrication Techniques.
The fabrication techniques of the Soviet aircraft industry
are vastly different from current US techniques and, in general, can
be said to be equivalent to US techniques in World War II. This has
a great bearing on the types of materials used since the ability to
handle certain materials is dependent upon modern tooling and a large
skilled labor supply. There is a great difference between the fab-
ricating techniques of airframe production and aircraft engine
production in the USSR.
The
RD-45 engine indicated the utilization
of extensive tooling, highly skilled labor, and critical casting and
forging techniques in its manufacture. 2/ Examination of later
MIG-15's indicates the same differences in manufacturing techniques.
This can be explained by the fact that aircraft engine manufacture is
largely done by standard machine tools, whereas airframe manufacturing
requires many large, special-purpose machine tools under present US
production technique. The Russians have apparently been unable to
reequip airframe plants with modern machine tools and, until the
plants are so equipped, they cannot efficiently employ new materials
such as magnesium sheet and 75 ST aluminum.
B. Materials Usage.
1. Major Materials.
The Soviet aircraft industry employs aluminum alloy sheet,
castings, and forgings in the manufacture of airframes and aircraft
engines. The industry uses large quantities of 24 ST type sheet and
only limited quantities of the 75 ST type. 3/ Aluminum castings and
forgings rather than magnesium castings are used most frequently for
the manufacture of aircraft engines. 4/ the
Soviet rejection rate of raw castings is2 to 4 times that of US
industry. 5/ Aluminum alloy forgings are used to the largest extent
in the manufacture of reciprocating aircraft engines for such parts as
crankcases and pistons. 6/
Steel is used extensively in both airframes and aircraft
engines by the Russians. A standard structural steel, Cromansil, is
employed almost exclusively for the construction of airframes. I/ In
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fabricating this steel for airframe components, a great preference
is shown for building up the desired shape using weldments. 8/ For
the steel parts of reciprocating aircraft engines the Russians use
the Wright Aeronautical Corporation pre-World War II Bill of
Materials for the respective aircraft engines. 9/ The selection of
steels for the Soviet jet engines indicates the maturity of Soviet
aircraft metallurgy. Materials have been used in conformance with
US, UK, German, or native practices, depending always on the most
economic material. 10/ In general, the Russians use more steel in
airframes than 40 US manufacturers.
In addition to use in electrical wiring and as an alloy-
ing element, copper is used by the Russians in a lead-bronze, anti-
friction alloy extensively used as a bearing material. 11/
Magnesium is employed much less for airframe and aircraft
engine components in the USSR than in the US. It is used in a cast
form only in low-strength applications. There is no evidence of the
employment of magnesium sheet in the Soviet aircraft industry. 12/
Little significance can be attributed to the limited application of mag-
nesium in the aircraft material examined to date, since these exami-
nations have been confined to Soviet fighter aircraft. The weight
savings gained by the use of magnesium are more critical in the
construction of heavy-bomber aircraft, and in the US, magnesium alloys
are assuming increased importance principally in this field. Thus it
Is anticipated that examination of Soviet heavy-bomber aircraft should
reveal a more extensive application of magnesium.
The principal use of lead, other than as an alloying
element, in the Soviet aircraft industry is in the fabrication of mass-
balances that are inserted in the airframe for static and dynamic
stability purposes. 13/
Natural rubber and synthetic types, namely, polybutadiene
nitrile and polychloroprene, are employed by the Russians for various
parts of their aircraft such as tires, flexible hoses, 0-rings, and
fuel-tank sealants. The Russians have had the capability of producing
satisfactory synthetic rubber aircraft products since the outbreak of
World War II. 14/
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Glass is used by the Russians' in the manufacture of
bullet-resistant windshields. Examination of material indi-
cates that the Soviet bullet-resistant plate iB manufactured by
laminating 1.25-inch acrylic sheet to 1-inch plate glass. 15/ The
major use of plastics by the Soviet aircraft industry is in the
manufacture. of clear acrylic canopies. 16/
2. Substitute Materials.
Substitution of raw materials in the Soviet aircraft
industry involves substituting one element for another when alloying
or compounding a material to meet a given specification. There are
many instances of this metallurgical substitution in the USSR, and
the resultant quality has been varied
. In all cases examined, the quality of
substituted materials has been sufficient for the application in-
tended and in isolated cases has yielded a material with superior
characteristics to anything known in the West.
The assumption can safely be made that the Russians will
try to conserve nickel, columbium, cobalt, zinc, molybdenum, and
copper; Specific instances where savings might be effected are dif-
ficult to point out. The question of what substitutions are foreseen
can best be answered by reviewing what has been found in Soviet air-
frames and aircraft engines. The following examples are cited:
a. In 1949 the Russians used an alloy very similar to
G-18-B in the manufacture of the turbine rotor disc for the RD-45
engine. They used 66 percent less columbium and 25 percent less
nickel, however,, than was used by the UK and the US. Creep and
stress rupture tests of this alloy reveal that the Soviet composi-
tion was 600 psi superior at actual operating conditions. If the US
had made approximately the same reductions, 19,000 pounds of colum-
bium and 28,000 pounds of nickel would have been saved during 1953
on the J-48 program alone. 17/ In later models ofSoviet jet engines,
the G-18B type alloy was changed to a ferritic composition resulting
in further savings of these critical elements. 18/
b. The Russians have successfully employed aluminized
carbon steels in place of stainless steel in the outer combustion
chambers of the RD-45 and VK-1 jet engines. This substitution is now
being adopted by the US industry, and the elimination of type 321
stainless steel in such application is estimated to conserve approx-
imately 150,000 pounds of chromium and 66,00o pounds of nickel per
year. 19/
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c. The Russlans.Used Type 321 stainless steel in the tur-
bine exhaust flange, the turbine nozzle-vane inner-shroud support, and
the turbine case of the RD-45 jet engine instead of H.R. Crown Max
which contains a much higher percentage of chromium and nickel and
about 3 percent tungsten. This substitution was made without appar-
ently impairing efficiency or operating life. The Russians retained
H.R. Crown Max in hotter parts of the engine. 20/
d. Soviet studies and actual application of boron-treated
steels to increase hardenability indicates that the USSR can conserve
nickel, molybdenum, and vanadium by this technique. This trend is
confirmed by the wide usage of boron-treated Cromansil types of steel
that have been found in every airframe and aircraft engine examined
to date. 21/
The only known use of cobalt in the Soviet aircraft
industry is in turbine guide vanes and turbine blades of the VK-1 jet
engine. The main use of cobalt in US reciprocating engines is in
the alloy used for facing valve seats and in the alloy used ih the
valve tips. Materials analysis of the valves from a Soviet ASH-62-
aircraft engine indicated an absence of cobalt. 22/ The valve tip
alloy used by the Wright Aeronautical Corporation contains from
2.7 to 3.3 percent cobalt; the Soviet materials contain none. The
World War II US specifications for valve seat alloys required a
cobalt-chromium alloy containing from 50 to 55 percent nickel. 23/
Current US practice utilizes an 80 nickel-20 chromium-type alloy. 24/
The absence of cobalt from the seat alloy and the use of an alloy
containing only about 50 percent nickel indicate that the course of
Soviet development work in the valve material field may have been
guided by a need to conserve both cobalt and nickel. Since the
analysis of the reciprocating engine parts have revealed
the absence of cobalt, the assumption is made that the Russians do
not use cobalt alloys in their reciprocating engines.
Based on the examples cited above, the conclusion is
reached that the Russians will make aggressive efforts to downgrade
the critical-element content of their aircraft alloys. The Russians
acted to save critical materials in their jet engines before the US
did in similar engines. The critical elements that the Russians
will attempt to conserve are nickel, columbium, cobalt, zinc,
molybdenum, and copper.
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C. Method of Computing Materials Inputs.
1. Airframes.
The materials input requirements for Soviet airframes and
aircraft engines have been estimated principally by analogy with
comparable US types.
transported to the US to be analyzed and studied by the ATIC and
the Cornell Aeronautical Laboratory, Inc., at Buffalo, New York.
From a study of this aircraft, a compilation of the rough stock re-
quired to produce one MIG-15 airframe was assembled. 25/ Estimates
were made of the wing group, empennage, and main landing gear, which
were in poor condition. In the final summarization, where the
weights of some materials were low in comparison with US fighters,
these rates were adjusted upward to produce a more realistic figure.
Cornell did not include scrap losses in the rough stock
bill of materials for the MIG-15. Soviet scrap losses, however, are
not assumed to be any greater than those experienced in the US for
the following reasons:
a. The standards of Soviet workmanship in non-critical
areas are lower than the standards accepted in US practice.
b. Hand labor is used, making possible reworking of
rejected parts and usage of trim-off materials.
c. Regulations of the People's Commissariat for Trade
impose heavy fines on the worker for materials spoilage. 26/
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The first discrepancy to be noted in the MIG-15 bill of
materials as calculated by Cornell was the wide proportionate dif-
ference between the materials input requirements to produce the MIG-15
and the F86E airframe. Materials weighing 7,117 pounds are required
to produce 1 MIG-15 with an Aeronautical Monthly Progress Report (NPR)
airframe weight* of 5,130 pounds; but 14,021 pounds of materials are
required for 1 F86E with an AMFR airframe weight of 7,216 pounds.
According to US aircraft industry practice, 10 to 30 percent of the '
quantities shown in bills of materials are added for contingencies. 27/
Assuming that these same contingencies exist in Soviet practice, ATIC
adjusted the Cornell value upward by 15 percent. Since the US bills
of materials include approximately 10 percent scrap, ATIC further
increased the MIG-15 gross input value by this amount. These adjust-
ments brought the MIG-15 input quantities to a total of 8,890 pounds,
which is more in line with US values.
* AMTR airframe weight is defined as follows:
Weight empty (weight of aircraft minus crew, fuel, oil, armament,
cargo, bombs, and disposable or special equipment) minus the total
weight of the items listed below:
1. Engine (dry weight).
2. Propeller hubs, blades, power control, and governor.
3. Wheels, brakes, tires, and tubes.
4. Auxiliary power plant.
5. Turbosupercharger (not including controls, intercoolers,
lubricating system, and similar equipment).
6. Radio receivers, transmitters, radar and removable units
(but not installation parts and wiring).
7. Starter (not including shafts, gear boxes, wiring, and similar
equipment).
8. Battery (not including containers or other items).
9. Generator (not including control boxes, regulator, and similar
equipment).
10. Turrets, and power operated gun mounts. If the plant manu-
factures its own turrets, the weight of the turret is not
included in this item.
AMPR airframe weight of a helicopter is the same as defined above
except that item 2 is omitted from the list of items to be deducted
from airframe weight empty. In effect, this means that rotors, as well
as the rotor-driving mechanism (includes transmissions, clutches,
shafting) and free wheeling units for main and tail rotors), should be
included in the airframe weight of helicopters.
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In the case of the Type 39 (latest variation of the
MIG-15), gross materials inputs were derived by multiplying the ma-
terials requirements for the MIG-15 by the ratio of AMPR airframe
weights of the .Type 38 to the MIG-15.
Gross materials input values for Soviet aircraft (11-28,
Type 35, Tu-41 11-12, Li-2, Yak-6, Yak-8, Yak-16, Yak-11, Type 33,
Type 34, Omega I, Type 32, and Type 36) were derived by multiplying
the ratio of USSR airframe weights to US AMPR airframe weights times
the gross materials input required for the US aircraft equivalent.
Quantities of aluminum, steel, copper, and other materials for Soviet
aircraft were derived by using this same ratio, with the exception of
the 11-28 and the Type 35.
In the cases of the 11-28 and the Type 35, ATIC substituted
adjusted percentages of aluminum, steel, copper, and other materials
for the B-57 (the comparable US aircraft) percentages: 28/ The-ad-
justed values were considered more realistic in view of the relatively
high percentage of steel used in the MIG-15 compared with the average
US percentages of steel used,
The US bills of materials do not include materials for
landing gears. The Air Materiel Command, Wright-Patterson Air Force
Base, Ohio, could only furnish the gross materials input require-
ments for the landing gear of two US counterparts. These gross
inputs were proportional to the gross requirements for the landing
gear of the MIG-15. Hence, the gross requirements for the other air-
craft were increased by the following amount:
MIG-15 landing gear material input AMPR airframe weight
MIG-15 AMPR airframe weight -x of aircraft noted
Complete bills of materials were not available on US air-
craft comparable to the An-2, Yak-12, Yak-18, and Type 25. In these
instances the gross materials input value was derived as follows:
MIG-15 gross input AMPR airframe weight
MIG-15 AMPR airframe weight of aircraft noted
ATIC assigned arbitrary percentages of aluminum, steel,
and other materials to these gross materials inputs to derive an esti-
mate, since these percentages were approximately in line with US values
for comparable aircraft.
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The Russians use almost exclusively a standard struc-
tural steel, Cromansil, for airframes. Hence, the percentages of
low-carbon steel and stainless steel are very low. 29/ The US bills
of materials contained relatively-larger percentages of low-carbon
steel and stainless steel than are contained in the MIG-15 bill of
materials. The ratios of low-carbon steel and stainless steel to
the gross amount of steel of the MIG-15 were used to estimate the
amount of these alloys in the bills of materials for the other Soviet
aircraft.
The design decision made with regard to the use of steel
or aluminum is a function of a complex set of interdependent vari-
ables. These variables include design traditions, aerodynamic con-
siderations, economic factors such as materials availability, and
manufacturing problems such as machine tools, equipment, and labor
skills available. Each of these variables influences the design
decisions made. In the US, design traditions and aircraft per-
formance specifications would probably have the major influence on
design decision. In the USSR the availability of materials, machine
tools, equipment, and labor skills would probably have a greater
influence than in the US. In general, US data indicate a tendency to
minimize the ratio of steel to aluminum whereas Soviet designers
would probably tend to maximize the ratio.
Although the use of a relatively high percentage of steel
may be favored in larger Soviet aircraft such as the Tu-4, practical
considerations of performance efficiencies of larger aircraft and
factors such as rigidity and aerodynamic loads would limit the amount
of steel which would be used. The ratio of steel to aluminum with
regard to Soviet aircraft might be expected to remain higher than in
US aircraft; therefore, derived Soviet gross materials input require-
ments listed in Table 2* could be considered as representing the
minimum requirements for steel. There are insufficient Soviet data
at present to adjust Soviet percentages of steel, aluminum, and
other materials above those listed. Closer examination by ATIC of
materials applications in the Yak-11 will provide some clue as to the
Soviet pattern?
* Table 2 follows on p. 16.
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Table 2
Bills of Materials for Soviet Airframes
1953
Pounds
Input
Type of Aircraft
Fighter
Bomber
Transport
Trainer
Recon-
naissance
Rotary Wing
Glider
Type
38
MIG-
15
11-28
Type
35
Tu-4
An-2
11-12
Li-2
Yak-6
Yak-8
Yak-
12
Yak-
16
Yak-
11
Yak-
18
Type
33
Type
34
Omega
I
Type
32
Type
36
Type
24
Airframe Weight
7,000
5,130
16,840
17,000
48,114
3,500
16,000
13,370
1,754
2,394
807
5,946
2,500
850
5,040
20,500
1,500
2,300
4,710
6,300
Low-Carbon Steel
336
245
707
- 714
1,300
119
400
361
96
126
27
137
63
29
66.
267
152
232
476
170
Alloy Steel (Not including
Stainless Steel)
5,820
4,270
12,160
12,280
22,870
2,098
6,780
6,280
1,666
2,180
483
2,420
1,063
492
2,027
4,450
2,612
4,005
8,200
2,887
Stainless Steel
55
40
115
116
212
20
64
59
16
20
5
23
10
5
10
41
24
37
75
27
Aluminum
5,170
3,790
21,210
21,420
54,400
3,540
21,760
11,740
1,144
1,561
815
6,480
3,575
900
6,300
24,400
1,575
2,415
4,950
7,250
Copper and Copper Base
Alloys
392
289
741
748
1,588
130
592
308
121
158
30
244
75
35
96
349
110
168
344
183
Magnesium
23
17.
66
66
149
0
352
160
0
0
0
71
45
0
00
0
475
729
1,490
0
Lead
48
35
34
34
481
16
400
40
5
7
4
18
0
4
25
103
0
0
0
21
Rubber
94
69
1,044
1,054
1,636
30
784
388
51
67
7
172
63
7
202
820
18
28
57
41
Glass and Plastics
136
, 100
118
119
914
46
208
173
23
.30
10
77
40
11
116
471
36
55
133
62
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The materials input coefficients for the Soviet airframes
were derived by dividing the input requirement in Table 2 by the
AMPR airframe weights. The coefficient may be expressed as the fol-
lowing ratio:
Pounds of material per unit airframe
Pounds of AMPR airframe weight
The materials input coefficients for the Soviet airframes are presented
in Table 3.*
2. Aircraft Engines.**
ATIC examinations of Soviet aircraft engines have not re-
vealed any significant quantitative differences in materials applica-
tions compared to their US counterparts. The bills of materials for
equivalent US aircraft engines were used for the Soviet aircraft
Table 3 follows on p. 19.
** The integral parts of an aircraft engine are as follows:
a. Reciprocating Engines.
The integral parts of reciprocating engines include: integral
supercharger, propeller reduction gears, integral engine lubrication
system, oil pumps, starter connection including starter dog, gun syn-
chronizer, impulse generator drive, generator or power take-off drive,
vacuum and hydraulic pump drives, propeller governor drive, and all
piping and controls between engine parts. The integral parts do not
include: ignition system (complete), carburetor, aftercoolers and
intercoolers, fuel injection system, starter, generator, and fuel
-pumps.
b. Jet Engines.
The integral parts of jet engines include: accessories gear
case assembly, all accessories except those designed and manufactured
by vendors, compressor assembly, turbine stator assembly, exhaust cone
assembly, and, where applicable, propeller gear box, as well as all
piping required in the engines themselves as inherent power plant
carriers to the point of quick disconnects located in the airframe.
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engines without adjustment with the exception of the R1300-1, the US
equivalent of the Soviet ASH-21. No magnesium is used in the
ASH-21. 30/ Therefore, the amount of aluminum required for the R1300-1
was increased by the amount of magnesium required. The gross inputs
for the Soviet aircraft engines were derived by multiplying the ratio
of Soviet to US aircraft engine dry weights* times the materials input
values for the equivalent US aircraft engine. The gross materials input
requirement for each Soviet aircraft engine is listed in Table 4.**
The materials input coefficients for Soviet aircraft engines
were computed from the following relationship:
Pounds of material per unit engine
Pounds of engine dry weight
The materials input coefficients for the Soviet aircraft engines are
given in Table 5.***
D. Materials Requirements.
1. Airframes.
The materials requirements for airframes were esttmarted
by multiplying the coefficients of Table 3 by the total pounds pro-
duced. The .materials inputs required by type of aircraft are shown
in Table 6.**** The materials requirements to meet current production
and assumed capacity production in 1954, 1955, and 1956 are pre-
sented in Appendix A for each airframe plant. In case the Russians
tried to produce at capacity, the assumption was made that the wou d
not continue to produce the models being produced in Plants
nce
models that would be produced in these plants under capacity condi-
tions are unknown, the number of aircraft being produced was determined
from the weighted average airframe weight of the known aircraft in
production. In estimating the materials inputs for the above plants,
the Tu-4 coefficients were used and an average of the
MIG-15, 11-28, 11-12, and Li-2 coefficients was used for the other
plants. The gross materials requirements of the Soviet airframe
industry are summarized in Table
* Engine dry weight is
integral parts of an aircraft
** Table 4 follows on p.
defined as the weight of the assembled
engine minus lubricants.
20.
***
Table
5 follows on p.
20.
****
Table
6 follows on p. 21.
Table
7 follows on p.
23.
xxx**
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Table 3
Materials Input Coefficients for Soviet Airframes it/
1953
Type of Aircraft
Fighter
Bomber
Transport
Trainer
Reconnaissance
Rotary Wing
Glider
Input
Type
38 MIG-15
11-28
Type
35
Tu-4
An-2
I1-12
L1-2
Yak-6
Yak-8
Yak-12
Yak-16
Yak-11
Yak-18
Type
33
Type
34
Omega
I
Type
32
Type
36
Type
24
?
Low-Carbon Steel
0.048
0.048
0.042
0.042
0.027
0.034
0.025
0.027
0.055
0.055
0.034
0.023
0.025
0.034
0.013
0.013
0.101
0.101
0.101
0.027
Alloy Steel (Not including
Stainless Steel)-
0.832
0.832
0.722
0.722
0.475
0.599
0.424
0.470
0.950
0.950
0.599
0.407
0.425
0.579
0.402,
0.217
1.741
1.741
1.741
0.458
Stainless Steel
0.0078
0.0078
0.0068
0.0068
0.044
0.0056
0.0040
0.0044
0.0089
0.0089
0.0056
0.0038
0.0040
0.0054
0.0020
0.0020
0.016
0.016
0.016
0.0043
Aluminum
0.739
0.739
1.26
1.26
1.13
1.01
1.36
0.878
0.652
0.652
1.01
1.09
1.43
1.06
1.25
1.19
1.05
1.05
1.05
1.17
Copper and Copper Base
Alloys
0.056
0.056
0.044
0.044
0.033
0.037
0.037
0.023
0.069
0.069
0.037
0.041
0.00
0.041
0.019
0.017
0.073
0.073
0.073
0.029
Magnesium
Lead
0.0033
0.0068
0.0033
0.0068
0.0039
0.002
0.0039
0.002
0.0031
0.001
0.0
0.0046
0.022
0.025
0.012
0.003
0.0
0.00
0.0
0.003
0.0
0.0046
0.012
0.003
0.018
0.0
0.0
0.0046
0.0
0.005
0.0
0.005
0.317
0.0
0.317
0.0,
0.317
0.0
0.0
0.034
Rubber
0.0135
0.0135
0.062
0.062
0.034
0.0087
0.049
0.029
0.029
0.029
0.0087
0.029
0.025
0.0087
0.040
o.04o
0.012
0.012
0.012
0.0065
Glass and Plastics
0.0195
0.0195
0.007
0.007
0.019
0.013
0.013
0.013
0.013
0.013
0.013
0.013
0.016
0.013
0.023
0.023
0.024
0.024
0.024
0.0098
a. Materials input coefficient= Pounds of material per unit airframe
Pounds of AMPR airframe weight
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Table 4
Bills of Materials for Soviet Aircraft Engines a/
1953
Pounds
Type of Aircraft Engine
Input
Jet
Reciprocating
VK-1
(Improved)
VK-1
ASH-90
ASH-82
ASH-62
ASH-21
M-11
Dry Weight
2,010
1,980
2,960
1,980
1,189
1,077
429
Low-Carbon Steel
422
416
459
194
1,617
227
931
Alloy Steel (Not including
Stainless Steel)
923
909
7,580
5,980
2.,222
2,520
592
Stainless Steel
2,030
2,000
1,009
0
0
168
0
Aluminum
1,646
1,622
2,410
1,339
503
1,088
280
Copper and Copper Base Alloys
12
12
358
190
87
60
61
Magnesium
0
0
0
48
0
0
0
Cobalt
58
57
0
0
0
0
0
a. The above bills of materials include scrap and reject losses but do not include spares.
Table 5
Materials Input Coefficients for Soviet Aircraft Engines a/
1953
Type of Aircraft Engine
Jet
Reciprocating
VK-1
Input
(Improved)
VK-1 ASH-90 ASH-82 ASH-62 ASH-21
M-11
Low-Carbon Steel
0.210
0.210 0.155 0.098 1.36 0.211
2.17
Alloy Steel (Not including
Stainless Steel)
0.459
0.459 2.56 3.02 1.87 2.34
1.38
Stainless Steel
1.01
1.01 0.341 0.0 0.0 0.156
0.0
Aluminum
0.819
0.819 0.814 0.676 0.423 0.01 ?
0.652
Copper and Copper Base Alloys
0.0059
0.0059 0.121 0.096 0.073 0.056
0.142
Magnesium
0.0
0.0 0.0 0.024 0.0 0.0
0.0
Cobalt
0.029
0.029 0.0 0.0 0.0 0.0
0.0
a. Materials input coefficient = Pounds of material per unit engine.
Pounds of engine dry weight
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Table 6
Gross Materials Requirements for Production of Soviet Airframes
1953
Model
Airframes Produced
(Units)
Airframes Produced
including Spares
(Pounds)
Low-Carbon Steel
(Metric Tons)
Alloy Steel, Not
including Stainless Steel
(Metric Tons)
Stainless Steel
(Metric Tons)
Aluminum
(Metric Tons)
Copper and Copper
Base Alloys
(Metric Tons)
Magnesium
(Metric Tons)
Lead -
(Metric Tons)
Rubber
(Metric Tons)
Glass and
Plastics
(Metric Tons)
Fighter
MIG-15 or
Variant
Bomber
11-28 .
Type 35
Tu-4
3,980
1,008
384
312
30,580,000
18,600,000
7,200,000
16,234,000
666
354
137
199
11,500
6,090
2,360
3,500
108
57.4
22.2
32.4
10,300
10,600
4,120
8,320
777
371
144
243
45.8
32.9
12.7
22.8
94.3
16.9
6.5
7.4
187
523
202
250
270
59.0
22.9
140
Transport
An-2
132
558,000
8.6
152
1.4
256
9./1
0.0
1.2
2.2
3.3
11-12
70
1,406,000
16.0
271
2.6
868
23.6
14.0
16.0
31.3
8.3
Li-2
135
2,318,000
28.4
494
4.6
; 923
24.2
12.6
3.2
30.5
13.7
yak-6
324
723,000
18.0
312
2.9
214
22.6
0.0
1.0
9.5
4.3
Yak-8
240
723,000
18.0
312
2.9
214
22.6
0.0
1.0
9.5
4.3
Yak-12
240
240,000
3.7
65.2
0.6
110
4.0
0.0
0.5
0.9
1.4
Yak-l6
192
1,446,000
15.1
267
2.5
715
26.9
7.9
2.0
19.0
8.5
Trainer
Yak-11
312
987,000
11.2
190
1.8
640
13.4
8.1
0.0
11.2
7.2
Yak-18
1,416
1,499,000
23.1
394
3.6
721
27.9
0.0
3.2
6.o
8.8
Reconnaissance
Type 33
133
843,000
5.0
154
0.8
478
7.3
0.0
1.9
15.3
8.8
Type 34
44
1,127,000
6.6
111
1.0
608
8.7
0.0
2.6
20.4
11.8
Rotary Wing
Type 36
55
324,000
14.8
256
2.4
154
10.7
46.6
0.0
1.8
3.5
Glider
Type 24
360
2,886,000
35.3
690
5.6
1,530
38.0
0.0
4.4
8.5
12.8
' Total
9,337
87,694,000
1,560
27,000
253
40,800
1,770
203
162
1,330
589
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Table 7
Gross Materials Requirements of the Soviet Airframe Industry
1953 Production and 1954-56 Capacity
Metric Tons
Input
1953
Production
Capacity Production
1954
1955
1956
Low-Carbon Steel
Alloy Steel (Not including
1,560
3,280
5,900
7,020
Stainless Steel)
27,000
56,600
102,000
121,000
-Stainless Steel
253
532
955
11140
Aluminum
40,800
87,900
155,000
186,000
Copper and Copper Base Alloys
1,770
3,700
6,650
7,960
Magnesium
203
469
863
1,090
Lead
162
444
823
1,060
Rubber
1,330
2,980
5,200
6,24o
Glass and Plastics
589
1,250
2,250
2,690
2. Aircraft Engines.
The estimate of gross material inputs given in Table 8*
for each type of aircraft engine was obtained by multiplying the
coefficients of Table 5** by the pounds of engines produced. The
estimate of aircraft engine production 32/ was based on the number of
engines required to support the current production of aircraft, the
assumption being that 125 percent spare engines are required for each
engine installed in an aircraft. Since the production of aircraft
engines was estimated by this method and not by an estimate of the
production of each engine plant, no estimate of the materials required
by individual plants was made.
* Table 8 follows on p. 24.
** P. 20, above.
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Table 8
Gross Materials Requirements for Production of Soviet Aircraft Engines
1953
Input
Unit
Type of Aircraft Engine
Jet
Reciprocating
Total
VK-1
(Improved)
VK-1
ASH-90
ASH-82
ASH-62
ASH-21
M-11
Engines Produced
Dry Weight Engines Produced
Low-Carbon Steel
Alloy Steel (Not including
Stainless Steel)
StainlesS Steel
.
Aluminum
Copper and Copper Base
Alloys
Magnesium
Cobalt
Units
Pounds
Metric Tons
Metric Tons
Metric Tons
Metric Tons
Metric Tons
Metric Tons
Metric Tons
601
1,208,000
115
251
554
449
3.2
0
1.6
15,219
30,100,000
2,880
6,290
13,800
11,200
80.8
0
396
2,808
8,310,000
584
9,650
1,290
3,070
456
0
0
513
1,020,000
45.4
1,040
0
313
44.4
11.1
0
1,031
1,230,000
759
1,040
0
236
40.7
0
0
1,863
2,010,000
192
2,130
142
921
51.1
0
0
6,264
2,690,000
2,650
1,680
0
795
/73
o
0
27,698
45,400,000
7,110
22,200
15,200
16,500
846
11.1
396
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As the production of aircraft engines has been estimated
from the number of aircraft, the number of engines at capacity pro-
duction will increase over the number at 1953 production by the same
percentage that the aircraft increase, assuming that the product mix
of aircraft remains constant. If the further assumption is made that
the product mix of engines will remain the same, the materials re-
quirements for capacity production may be estimated by multiplying
the materials inputs for 1953 production by the percentage increase
in number of aircraft; that is, increasing the current materials in-
puts by 2.12, 3.78, and 4.53 gives the materials requirements at
capacity production for 1954, 1955, and 1956, respectively. The
gross materials requirements for the number of aircraft engines to
support 1953 production and 1954-56 capacity production of aircraft
are given in Table 9.
Table 9
Gross Materials Requirements of the Soviet Aircraft Engine Industry
1953 Production and 1954-56 Capacity
Metric Tons
Input
1953
Production
Capacity Production
1954
1955
1956
Low-Carbon Steel
7,110
15,100
26,900
32,200
Alloy Steel (Not including
Stainless Steel)
22,200
47,100
84,000
101,000
Stainless Steel
15)200
32,200
57,400
68,900
Aluminum
16,500
35,000
62,400
74,800
Copper and Copper Base Alloys
846
1,790
3,200
3,830
Magnesium
11.1
23.5
41.2
50.3
Cobalt
396
840
1,500
1,790
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3. Summary.
The gross materials requirements for both Soviet airframe
and aircraft engine production are summarized in Table 10.
Table 10
Gross Materials Requirements of the Soviet Airframe
and Aircraft Engine Industries
1953 Production and 1954-56 Capacity
Metric Tons
Input
1953
Production
Capacity Production
1954
1955
1956
Low-Carbon Steel
8,670
18,400
32,800
39,200
Alloy Steel (Not including
Stainless Steel)
49,200
103,000
186,000
222,000
Stainless Steel
15,500
32,700
58,400
70,000
Aluminum
57,300
123,000
217,000
261,000
Copper and Copper Base Alloys
2,620
5,690
9,850
11,800
Magnesium
214
493
904
1,140
Lead
162
444
823
1,060
Rubber
1,330
2,980
5,200
6,240
Glass and Plastics
589
1,250
2,250
2,690
Cobalt
396
840
1,500
1,790
III. Labor.*
A. Characteristics of Soviet Plants.
Essential to any analysis of the capabilities of a production
facility is a thorough understanding of the efficiency of the labor
employed and the scale of effort currently being expended on the pro-
duction effort. The efficiency of labor normally means the produc-
tivity of a unit of labor in terms of the pounds of finished product
produced as compared to some standard productivity to be expected. ?
This efficiency as normally measured in terms of the pounds per
* The discussion of the labor force in the Soviet aircraft industry is
based primarily upon a study of the airframe plants although some of
the general conclusions doubtless apply to the aircraft engine plants
as well.
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man-hour produced can be compared either to recognized "standard"
hours established for each type of operation or can be compared to
the average pounds per man-hour of an equivalent industry. The
measure of labor efficiency in this report is taken to be the
average pounds produced per man-hour in the US aircraft industry in
1944. This standard has been acceptedysince such an average can be
computed from available statistics on US aircraft production during
World War II.
The over-all efficiency of labor in an aircraft industry is
affected by many different factorsywhich should be noted for the
purpose of full comprehension of the significance of the labor input
requirements of the Soviet aircraft industry. These factors can be
summarized as follows:
1. The size of plants.
2. The number and types of machine tools.
3. The fabrication techniques.
4. The organization and management.
5. The quality of aircraft design.
6. The number and quality of available workers.
7. The density of labor in the plant.
8. The hours per week worked by each employee.
To summarize briefly the conditions in the Soviet aircraft
plants pertaining to these factors, it can be said that Soviet plants
are generally considerably smaller than US plants, ranging in size from
0.5 million square feet to 2 million square feet, whereas many US
plants comprise as much as 5 million square feet. In like manner,
analysis of Soviet aircraft reveals that Soviet industry does not
utilize equivalent modern special-purpose machine tools found in US
plants and depends more upon hand fabrication and standard machine
tools. There is evidence, however, that Soviet airframe and aircraft
engine designs are comparable to US standards. The design philosophy
in the USSR differs from that of the US. Soviet aircraft design is
determined by the functional requirements, the size and type of pro-
duction facilities, the availability of materials, the desire for a
high production rate, and the availability of a large supply of un-
skilled labor, whereas in the US design would be primarily a consider-
ation of the functional requirements. The management of Soviet plants
is considered excellent. Soviet plants have been producing for at
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least 15 years and are characterized as self-sufficient, self-con-
tained units comparatively isolated from other plants because of
inadequate transportation facilities. The organization of all
plants is a standard organization established by the Ministry of
Aviation Industry, which also established standard worker norms
for the man-hours required to produce a given part. 33/
B. Types of Labor Required.
1. Skilled.
The labor force of the Soviet aircraft industry consists
of a large supply of unskilled labor, which leads to the practice of
greater reliance on hand fabrication than would be found in US plants.
Since all Soviet aircraft plants are classed as defense plants,
very few transfers of personnel are permitted from one plant to
another. The inexperienced laborer thus becomes the only source of
labor supply. Only 20 percent of the foremen in a plant are gradu-
ates of technical schools sponsored by the Ministry of Aviation
Industry. At least 90 percent of the workers work on a piecework
system and are categorized as follows:
Category 1.
Category 2.
Category 3.
Category 4.
Category 5.
Category 6.
Category 7.
Category 8.
Unskilled.
Laborers.
Laborers with some experience.
Persons who can maintain work without
continuous supervision but not com-
pletely qualified.
Persons completely qualified.
Qualified persons with outstanding
ability.
Specialized, highly qualified.
Specialized, requiring high degree
of training. Usually inspectors
and machine set-up men. 34/
The largest percent of direct workers belong to Categories 2 through
6, with a very small percentage in Categories 7 and 8. The per-
centage distribution of direct workers by principal categories in the
shops is as follows:
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Percent
Shop
Category
2
Category
3
Category
4
Category
5
Category
6 -
Category
7
Flight Test
0
0
25
25
35
15
Assembly
20
20
20
30
10
0
Riveting
Assembly
25
30
20
15
5
0
Fitting and
Welding
10
23
35
20
10
2
Sheet Metal
15
20
20
30
10
0
Machine
10
30
30
18
10
2.5 to
5
Workers in Categories 2 and 3 are primarily apprentices in machine
shops or in simple assemblies and comprise 35 percent of the direct
workers. Categories 4 and 5 comprise workers who have apprentices
working for them in the riveting assembly, sheet metal, and assembly
shops or who perform simple operations in the machine shop. This
group comprises about 48 percent of the direct labor. Thus from 80
to 90 percent of all direct workers belong to Categories 2 through 5.
Category 1 normally includes common laborers who are not working
directly on aircraft production.
By US standards, the difference between skilled and un-
skilled labor is primarily determined by the prevailin wage each
laborer receives and in turn is normally determined by the experience
ot' the laborer on the job. In effect, the required experience to
permit a laborer to draw a skilled laborer's wage is equivalent to
successful completion of apprenticeship on the job. If this defini-
tion of skilled and unskilled labor is applied to the categories given
above, the unskilled laborers would comprise Categories 1 through 4.
Taking Categories 5 through 8 as skilled, the percentage of skilled
laborers in the 6 shops listed above is 40 percent. The conclusion
is that, in Soviet airframe plants, the skilled labor force comprises
40 percent of the total direct labor force.
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The skilled labor force of a representative US aircraft
plant comprised 87 percent of the direct labor, 68 percent of the
indirect labor, and 8o percent of the total labor force. 35/ Assum-
ing that the same relationship of skilled indirect labor to skilled
direct labor exists in Soviet aircraft plants as existed in the US
plant, the Soviet skilled indirect labor comprises 31 percent of the
total indirect labor force.
Assuming that 50 percent of the total labor in Soviet
aircraft plants is direct labor, the skilled labor force comprises
35 percent of the total labor force in Soviet plants.
2. Direct.
Soviet airframe plants are roughly comparable to US air-
frame branch plants, since many functions performed by the parent
plant in the US are normally performed in Moscow for the entire
Soviet serial production airframe industry. Such functions include
engineering, contract administration, procurement, tool design, re-
search and technological development, and experimental production. 36/
Since these functions are performed by indirect labor, the ratio of
direct labor to total labor in Soviet airframe plants would tend to
be higher than in the US airframe industry. The ratio of direct
workers in US airframe branch plants, however, should be comparable
to that of Soviet plants. During World War II, in US airframe branch
plants subcontracting less than 50 percent, 53 percent of the total
labor was direct labor. 37/ (See Table 11.*)
Other factors, however, suggest that a more complex
organizational structure exists in Soviet plants than in US airframe
branch plants. Indications of this complexity are that each depart-
ment has its group devoted to timekeeping, bookkeeping, technical
control, inspection, time study, production control, and other groups
in addition to a centralized department devoted to these functions.
In addition, the following sections appear to have a more complex
organization than would be found in a US airframe branch plant:
* Table 11 follows on p. 31.
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Table 11
Ratio of Direct Labor to Total Labor
in US Airframe Branch Plants during World War II
US Airframe Branch Plants
Direct Labor as an
Average Percent of
Total Labor
Bell Aircraft Corporation, Marietta, Georgia 42.9
Boeing Airplane Company, Inc., Wichita, Kansas 52.6
Consolidated Vultee Aircraft Corporation,
Downey, California 62.7
Consolidated Vultee Aircraft Corporation,
Fort Worth, Texas 57.6
Consolidated Vultee Aircraft Corporation,
Nashville, Tennessee 44.4
Consolidated Vultee Aircraft Corporation,
Wayne, Michigan 44.4
Curtiss-Wright Corporation, Buffalo, New York 52.6
Curtiss-Wright Corporation, St. Louis,
Missouri 56.0
Douglas Aircraft Company, Inc., Chicago,
Illinois 52.1
Douglas Aircraft Company, Inc., Long Beach,
California 59.0
Douglas Aircraft Company, Inc., Oklahoma City,
Oklahoma 51.4
North American Aviation, Inc., Dallas, Texas 59.4
North American Aviation, Inc., Kansas City,
Kansas 52.4
Average 52.9
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a. Air and Chemical Attack Defense Section.
b. Plant Secret Section.
c. Plant Internal Security Section.
d. Workers Training Section.
e. Workers Supply Section.
f. Workers Housing Section.
g. Transport Section.
h. Storage Section.
The Soviet plant organization also includes political
functions which have no counterpart in US plants. These functions
include the Plant Komsomol Committee and the Communist Party
Committee.
If Soviet plants are considered roughly comparable to US
airframe branch plants, and a ratio of 0.53 for direct to total
workers therefore will apply, then the other considerations given
above would tend to lower this ratio. For the purpose of this report,
a ratio of 0.50 for direct to total workers in Soviet airframe plants
is assumed.
No constant ratio of direct to total employees existed,
however, in the US airframe branch plants listed in Table 11. The
ratio of direct to total employees varied from month to month. Eight
of the 13 plants started with a ratio higher than the average of 0.53,
and 9 of the plants ended with a ratio higher than the average. In
these 13 US plants, the average range of the ratio of direct to total
employees was 0.39 to 0.67. For a period of 12 months, however, an
average figure should give fair results.
3. Managerial.
In an effort to determine what percentage of the total
labor force is engaged in management and administration, a study of
organization charts 38/ which are understood to apply to the airframe
industry rather than to a particular plant was undertaken. Using the
departments on which the source gave employment figures, the con-
clusion was reached that management personnel comprised 20 percent
of the total labor force. The term "management personnel" as used in
this report is synonymous with administrative personnel and includes
all personnel whose activities are concerned with the initiation of
an enterprise; the establishment of major policies; the provision
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of necessary equipment; the actual work of executing the objectives
for which the plant has been organized; the issuance of orders con-
cerning the work to be done; seeing that the personnel are fitted for
the work and trained to operate efficiently; and caring in general
for the everyday routine necessary to insure that men, materials, and
equipment are working toward the desired end. A management force
comprising 20 percent of the total labor force is high in comparison
to US airframe branch plants, but this figure is considered reason-
able for Soviet plants because of the more complex organization
structure, the duplication of effort, and the fear psychology which
pervades the industry.
4. Technical.
Further examination of the organization charts 39/ re-
vealed that 18 percent of the total labor force was technical
personnel. The term "technical personnel" as used in this report
comprises professional men, designers, and draftsmen. The percentage
of technical personnel in Soviet aircraft plants is about twice that
of US aircraft plants which may result from the following factors:
a. The Soviet classification of technologists may
include laboratory technicians.
b. Soviet plants do their own foundry and forge
work; hence, they require more metallurgists
than US plants.
c. Soviet plants do their own construction requir-
ing the use of civil engineers.
d. Greater duplication of technical functions
exists in Soviet plants than in US plants.
C. Worker Density.
Examination of indicates that shop methods
in Soviet aircraft plants making the MIG-15 closely parallel the
methods used during World War II in US fighter plants. 4o/ If the
Soviet shop methods are similar to those of the US during World War
II, then average floor space per worker should be equal in both
countries. A short supply of machine tools in Soviet airframe plants,
however, is assumed. 41/ The assumption therefore is made that be-
cause of the shortage of machine tools and the evidence of more hand
work, the average floor space per worker would be less in the Soviet
airframe industry than in that of the US.
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50X1
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A study was made of the relationship between floor space per
worker and airframe weight of the aircraft being produced in US
plants during World War II. No consistent relationship could be
determined, although there was a slight indication of larger floor
space per worker for heavier airframes.
Because no consistent relationship between worker density and
airframe weight could be determined and the shop methods used in the
fabrication and assembly of the MIG-15 are similar to those used in
the manufacture of the P-51, it was assumed that the floor space per
worker in a US branch plant making the P-51 would approximate Soviet
worker density. A study was made of the North American Aviation, Inc.
branch plant in Dallas, Texas. The average density over a period of
43 months was 135.6 square feet per total worker, whereas the
average density was 72.4 square feet per total worker for the 18 most
dense months. 42/ This density of 72.4 square feet is considered to
be representative of Soviet plants. Storage facilities in Soviet
airframe plants are estimated to occupy 3 percent more area than in
US branch plants. 43/ Therefore, the value of 72.4 square feet per
total worker was increased by 3 percent to account for the larger
storage area of the Soviet plants. The adjusted value of 75.0
square feet per total worker is assumed to be the worker density for
Soviet airframe plants.
Applying the shift factors of 100:70:50 44/ the following
densities are obtained:
Number of Shifts
Density (Square Feet of
Floor Area per Total Worker)
1
165.0
2
127.5
3
75.0
No constant worker density, however, exists in US airframe
plants. At the beginning of production of a new model, the floor
space per worker is large. As production accelerates and more
people are employed, the floor space per worker decreases until a
.peak-employment is reached, generally around the 18th month. If
production is held constant, labor requirements will decline in
direct proportion to the learning process, and the floor area per
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? ?
worker will begin to increase. It is believed that in Soviet airframe
plants, the workers would not be laid off as the labor requirements
decline; instead, the workers would be used to manufacture consumer
goods.
D. Labor Requirements.
1. Airframes.
Using the factors developed above, the labor requirements
of each Soviet airframe plant were estimated.- These labor require-
ments are presented in Appendix A. The labor requirements for.the
Soviet airframe industry are summarized in Table 12.
Table 12
Labor Requirements of the Soviet Airframe Industry
1953 Production and 1956 Capacity
Thousands of Workers
Type of Labor 1953 Production 1956 Capacity
Direct 86 201
Indirect 86 201
Total a/ 172
Skilled 60
Unskilled 112
Total a/ 172
Managerial b/ 34
Technical b/ 31
402
141
261
402
80
72
a. The categories direct and indirect and the cate-
gories skilled and unskilled represent different break-
downs of the same total.
b. For the explanations of these headings see pp. 32-33,
above.
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2. Aircraft Engines.
No employment study has been made of the Soviet aircraft
engine industry. However, if the assumption is made that the ratio
of total employment in the aircraft engine industry to total employ-
ment in the airframe industry is the same in the USSR as in the US,
a total employment figure for the Soviet aircraft engine industry
may be estimated. The US aircraft engine industry has employed an
average of 30.6 percent as many workers as the airframe industry
during 1947-52. 45/ Using this ratio and the same factors for
direct, indirect, skilled, unskilled, technical, and management
categories for the aircraft engine industry as were used for the
airframe industry, the labor figures for the aircraft engine industry
presented in Table 13 were estimRted.
Table 13
Labor Requirements of the Soviet Aircraft Engine Industry
1953 Production and 1956 Capacity
Thousands of Workers
Type of Labor 1953 Production 1956 Capacity .
Direct 26.5 61.5
Indirect 26.5 61.5
Total a/ 53.0 123.0
Skilled 19.0 43.0
Unskilled 34.0 80.0
Total a/
Managerial 12/
Technical 12/
53.0 123.0
11.10 25.0
10.0 22.0
a. The categories direct and indirect and the categories
skilled and unskilled represent different breakdowns of the
same total.
b. For the explanation of these headings, see pp. 32-33,
above.
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3. Summary.
The labor requirements for the Soviet airframe and
aircraft engine industries are summarized in. Table 14.
Table 14
Labor Requirements of the Soviet Airframe
and Aircraft Engine Industries
1953 Production and 1956 Capacity
Thousands of Workers
Type of Labor
1953 Production
1956 Capacity
Direct
112.5
262.5
Indirect
112.5
262.5
Total a/
225.0
525.0
Skilled
79.0
184.0
Unskilled
146.0
341.0
Total a/
225.0
525.0
Managerial b/
45.0
105.0
Technical b/
41.0
94.0
a. The categories direct and indirect and the
categories skilled and unskilled represent dif-
ferent breakdowns of the same total.
b. For the expanation of these headings, see pp. 32-33,
above.
An indication of labor efficiency in the Soviet aircraft
industry may be obtained by using the current direct labor figure of
86,000 workers estimated above and the current on-site production'
estimate of 6,380,000 pounds of airframe per month. 46/ Using the
factor of 48 work-hours per Soviet worker per week, 777 a Soviet
labor productivity of 0.361 pounds per direct man-hour is obtained.
In May 1944, the US peak labor productivity month, the employment
in the US airframe industry was 368,858 direct workers who worked an
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average of 45.8 hours per week, and the on-site production was
68,450,000 pounds of airframe. 48/ Thus the US produced 0.943
pounds per direct man-hour during the month of peak labor produc-
tivity. Using these labor productivity factors, the current Soviet
labor productivity is 38 percent of the 1944 US labor productivity
in airframe plants.
The US, however, produced 8o airframes per million
square feet of floor area in May 1944) and the current Soviet monthly
production is 25.9 airframes per million square feet of floor area.
It is obviously unfair to establish an efficiency that does not
account for the variation in the scale of production undertaken. In
the production of aircraft the cost of labor in man-hours per pound
of product decreases as production increases. In the US this
variation in man-hours per pound with quantity usually followed very
closely an 80-percent learning curve. In simple terms, the 80-per-
cent learning curve means that each time the quantity produced is
doubled, the unit of labor involved in production will drop to
80 percent of the amount required in the original quantity. Using
the 80-percent curve with rate of output as a base, the Soviet labor
productivity is found to be 0.524 direct man-hours per pound at the
rate of 80 airframes per month. Hence, the Soviet labor produc-
tivity is 56 percent of the 1944 US labor productivity.
In conclusion, it may be said that the labor force of the
Soviet aircraft industry is less efficient and less skilled than the
labor force of the US aircraft industry.
IV. Electrical Energy.
A. Scope.
An estimate of the total amount of electrical energy required
by the Soviet aircraft industry is made in this report, and no attempt
is made to estimate the percentage generated within individual plants.
B. Method of Estimating Electrical Energy Inputs.
The Soviet airframe plants probably use less electrical
energy than the average US airframe plant. This assumption is based
upon the indications that the Soviet airframe plants have a shortage
of machine tools and with few exceptions can'count only on standard
? machine tools smaller in size and capacity than the machine tools in
the average US plant. 49/
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? ? ? ? ? ?
Data on electrical energy consumption were obtained from 10
US airframe plants. In order to obtain an electrical energy input
coefficient for Soviet airframe plants, the data for the US plant
producing bombers with the lowest consumption of electrical energy
per square foot of floor area were used together with the data for
the lowest consumer of electrical energy among the fighter plants.
The average electrical energy consumption of these 2 plants was
8.95 kilowatt-hours per square foot per year for 1 shift. Using
the Soviet shift factors of 100:70:50, the following factors were
determined for use in determining electrical energy consumption in
Soviet airframe plants:
Scale of Effort
0.45
0.77
1.00
Electrical Input Factor
(Kilowatt-Hours per Square Foot per Year)
8.95
15.21
19.69
These electrical consumption factors may be considered the
minimum for Soviet airframe plants. The average electrical con-
sumption of the 10 US plants was 14.5 kilowatt-hours per square foot
of floor area per year for 1 shift or 1.62 times the average of the 2
lowest plants. Hence the electrical energy consumption of the Soviet
airframe plants could conceivably be 1.62 times the amount estimated.
Although a shortage of machine tools has been assumed for the
Soviet airframe industry, the indications are that the engine plants
employ fabrication methods similar to those used in the US. 50/ If
the aircraft engine fabrication methods are the same in the USSR as
in the US, it can be assumed that the electrical energy consumption
of the Soviet aircraft engine industry is equal to the consumption of
the US aircraft engine industry.
Data were available for the electrical energy consumption of
five US aircraft engine plants during World War II. The average con-
sumption of these 5 plants was 40.4 kilowatt-hours per square foot
per year at capacity. Therefore, this factor is used for the Soviet
aircraft engine plants when operating at a 100 percent capacity.
None of these five plants produced any jet engines. This average
consumption figure is considered a minimum figure, since there are
indications that a plant producing jet engines uses more electrical
energy than a plant manufacturing reciprocating engines. 51/
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C. Electrical Energy Requirements.
Using the consumption figures determined above, the electrical
energy requirements were determined for each Soviet airframe plant
for 1953 and capacity conditions. The results are presented in
Appendix A. The requirements for the industry are presented in
Table 15. These requirements are based upon the existing floor area.
However, under capacity conditions, the floor area would probably be
increased.
Table 15
Electrical Energy Requirements of the Soviet Airframe
and Aircraft Engine Industries
1953 Production and 1954-56 Capacity
Million Kilowatt-Hours
Electrical Energy Requirements
Aircraft Engine
Year Production Airframe Industry Industry Total
1953
254
165
419
1954 (Capacity)
593
338
931
1955 (Capacity)
593
604
1,200
1956 (Capacity)
593
719
1,310
The requirements of the Soviet aircraft engine industry are
also presented in Table 15 for both current and capacity conditions.
Using the aircraft engine methodology developed by CIA and assuming
no subcontracting, the aircraft engine industry would be operating
at a 23-percent scale of effort in order to support the current
production of airframes. The scales of effort required to support
capacity production of airframes in 1954, 1955, and 1956 are 47 per-
cent, 84 percent, and 100 percent, respectively. The above scales of
effort multiplied by the electrical energy consumption factor de-
termined above for aircraft engine plants were used to determine the
electrical energy requirements for the aircraft engine industry.
S -E-C -R-E-T
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V. Fuel and Lubricants..
A. Scope.
In addition to materials, manpower, and electrical energy,
other important inputs of the aircraft industry are coal, required
for heating plants, and lubricants used for machinery-lubricating
oils and grease and for cutting oils.
No estimate is made of the amount of coal that might be
used in generating electrical power'. Therefore, the estimate of the
coal requirement may be considered the minimum amount of coal re-
quired. No estimate has been made of the amount of fuel and lub--
ricants used in testing the aircraft and aircraft engines. The
amount of fuel and lubricants used in testing at the plant is insig-
nificant in comparison to that used for civil and military purposes.
B. Method of Determining Coal Input for Heating.
The heat-emitting devices of a heating plant for a factory
should be Capable of delivering a quantity of heat sufficient to
replace that transmitted through the structure and of heating the
air which enters plus an allowance for exposure to winds. The heater
should be able to supply the demands of the heat-emitting. devices,
service water heating) and other loads, plus an allowance for heat
losses from piping and ducts and for warming up from a cold start. In
general, heat is not required when the mean temperature for a 24-hour
period reaehes 65?F. When this temperature is used as a base, each
degree that the mean daily temperature is below 65?F is a degree-day
unit. As an example, a mean temperature of 25?F is 40 degree-day
units per day. The daily degree-day units are added for monthly
and yearly totals. Fuel consumption per square foot of radiation is
approximately proportional to the number of degree-day units.
The assumption is made that the coal consumption per square
foot of Soviet aircraft plants is equal to the following ratio:
Coal consumption per square foot x Degree-day units of Soviet plant
of US' plant Degree-day units of US plant
Fuel consumption data were obtained from 10 US plants, but the only
aircraft plant using coal for heating was the McDonnell Aircraft
Corporation in St. Louis, Missouri. This plant consumed an average
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of 23.3 pounds of coal per square foot per year while working two
shifts during 1951 and 1952. St. Louis, Missouri has 4,602 degree-
day units per year. 52/ The assumption was made that the same
amount of coal was consumed on each of the shifts worked and that
one-third of the amount required for a work shift was required for
an idle shift. Hence the following consumption factors were de-
termined for an aircraft plant in a locality having 4,602 degree-
day unts per year:
Number of Shifts Pounds of Coal Consumed
Worked per Square Foot per Year
1
16.7
2
23.3
3
30.0
The above factors together with the yearly degree-day units
for the Soviet plants were used to determine the amount of coal re-
quired by the Soviet airframe industry on the basis of a 6-day work
week. The aircraft engine plants would have to work only 1 shift.
5 days a week in 1957 to meet airframe production requirements. A
plant in a locality having 4,602 degree-day units and working on a
basis of 1 shift 5 days a week would consume 14.8 pounds of coal per
square foot per year.
A study of the coal consumption of individual plants in the
aircraft engine industry was not made. Instead, the ratio of the
total engine floor area to the total airframe floor area multiplied
by the amount of coal used by the airframe industry at capacity was
used to determine the 1956 aircraft engine industry requirementspat
which time the aircraft engine plants would be on 3 shifts 6 days a
week. The scale of effort for the aircraft engine plants in 1953
corresponds to 1 shift 5 days a week: therefore, the aircraft
engine plants would use 49.3 percent of the amount of coal used in
1956. In 1954 the aircraft engine plants would be on 1 shift for
6 days a week and would use 55.7 percent of the 1956 requirements.
In 1955 the aircraft engine plants would use 77.7 percent of the
1956 requirements.
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C. Method of Determining Lubricating Inputs.
Of the 10 US plants submitting data on the consumption of
electrical energy, of fuels, and of lubricants only 2 plants sub-
mitted data on the consumption of lubricating oils. These two plants
were the Republic Aviation Corporation and Northrop Aircraft, Inc.
In addition, Republic furnished data on lubricating grease and
Northrop supplied data on cutting oils. From these data, the fol-
lowing factors were determined:
Scale of Effort
(Percent)
Lubricating Grease
(Pounds per Square
Foot per Year)
Lubricating Oil
(Gallons per
Square Foot
per Year)
Cutting Oil
(Gallons per
Square Foot
per Year)
0.45
0.00313
0.0106
0.00392
0.77
.o.00532
0.0180
0.00666
1.00
o.00688
0.0233
0.00862
The lubricant inputs of the Soviet aircraft engine industry
are based upon the airframe industries' consumption of these inputs.
The manufadtUre of an aircraft engine involves more machine work than
does the manufacture of an airframe: therefore, an aircraft engine
plant should use more lubricants per square foot than an airframe
plant if both are working at the same capacity. The amount of elec-
trical energy consumed per square foot may be used to indicate the
amount of machine work. Assuming that the ratio of the consumption of
lubricants per square foot of floor area of an aircraft engine plant
to an airframe plant is approximately equal to the ratio of electrical
energy consumption per square foot, aircraft engine plants consume
2.05 times the lubricants consumed per square foot by airframe plants.
The consumption factors for lubricants for aircraft engine plants at
100-percent scale of effort is assumed to be as follows:
Lubricating Grease
Lubricating Oil
Cutting Oil
0.0141 pounds per square foot per year
0.0478 gallons per square foot per year
0.0177 gallons per square foot per year
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D. Fuel and Lubricants Requirements.
The amount of fuel and lubricants required by the Soviet
airframe and aircraft engine industries was estimated by the above
consumption factors. The requirements of these inputs for each air-
frame plant are presented in Appendix A. The coal and lubricants
requirements for the airframe and aircraft engine industries are
summarized in Table 16.*
VI. Transportation.
A. Scope.
Transportation inputs are discussed in terms of the total
tonnage of transportation required to support the production of each
plant and to distribute the final product to its ultimate destination.
B. Method of Estimating Tonnage to Be Transported.
1. Airframes.
The weight of components required for each aircraft was
estimated by subtracting the AMFR airframe weight plus the aircraft
engine dry weight from the empty weight of the aircraft. The amount
of scrap was determined by subtracting the pounds of airframe pro-
duced from the raw materials required. The assumption was made that
only the MIG-15, the Type 38, the Type 24, the Yak-11, and the Yak-18
aircraft would be crated and shipped from the plant; all other air-
craft are assumed to be flown away.
2. Aircraft Engines.
The weight of components required to be transported to
aircraft engine plants was assumed to be 2 percent of the total weight
of aircraft engines produced. The amount of scrap was determined by
subtracting the pounds of engines produced from the amount of raw
materials required.
* Table 16 follows on p. 45.
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Table 16
Fuel and Lubricants Requirements of the Soviet Airframe and Aircraft Engine Industries
1953 Production and 1954-56 Capacity
Amount
Capacity
1953 i954 1955 1956
Input
Unit
Airframes
Aircraft
Engines
Total
Airframes
Aircraft
Engines
Total
Airframes
Aircraft
Engines
Total
Airframes.
Aircraft
Engines
Total
Coal
Metric Tons
462,000
234,000
696,000
807,000
264,000
1,071,000
807,000
368,000
1,175,000
807,000
474?0oo
1,281,000
Lubricating
Grease
Metric Tons
4o
26.2
66.2
94
53.5
147.5
94
95.6
190
94
114
208
Lubricating
.
Oil .
Gallons
399,000
196,000
595,000
702,000
400,000
1,102,000
702,000
715,000
1,417,000
702,000
851,000
1,553,000
Cutting
Oil
Gallons
115,000
72,400
187,000
260,000
148,000
408,000
260,000
265,000
525,000
260,000
315,000
575,000
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C. Tonnage of Transportation Required.
1. Airframes
The tonnage of transportation required by each individual
airframe plant is presented in Appendix A. The total tonnage of
transportation required by the airframe industry is summarized in
Table 17.
Table 17
Transportation Requirements of the Soviet Airframe Industry
1953 Production and 1954-56 Capacity
Metric Tons
Products Transported
Products Transported to Plants from Plants
Raw Spare
Production Engines Components Materials Fuel Lubricants Aircraft Parts Scrap
1953
-
9,160
5,160
73,700
462,000
1,790
17,900
6,400
34,100
1954
(Capacity)
19,400
10,900
157,000
807,000
3,364
37,900
14,300
72,400
1955
(Capacity)
34,600
19,500
280,000
807,000
3,364
67,600
25,500
131,000
1956
(Capacity)
41,500
23,400
334,000
807,000
3,364
81,000
30,500
155,000
2. Aircraft Engines.
The tonnage of transportation required by the aircraft
engine industry is summarized in Table 18.*
VIT. Conclusions.
The conclusions that may be drawn from this report are as follows:
1. The USSR uses less critidal materials per pound of airframe
and aircraft engine weight than does the US.
* Table 18 follows on p. 47.
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Table 18
Transportation Requirements of the Soviet Aircraft Engine Industry
1953 Production and 1954-56 Capacity
Metric Tons
Products Transported to Plants
Com- Raw
Production ponents Materials Fuel
Lubri
cants
Products Transported
from Plants
Engines
Shipped
to Air-.
frame
Plants Spares Scrap
1953
412
61,900
234,000
939
9,160
11,400
41,300
1954
(Capacity)
874
131,000
264,000
1,920
19,400
24,300
87,300
1955
(Capacity)
1,560
234,000
368,000
3,430
34,600
43,200
156,000
1956
(Capacity)
1,870
281,000
474,000
4,090
41,500
51,800
188,000
2. The USSR will try to conserve critical elements such as
nickel, columbium, cobalt, zinc, molybdenum, and copper in the manu-
facture of airframes and aircraft engines. In conserving these
elements, the Russians will not lower the quality of any material that
can exert a significant bearing on the operational performance of the
aircraft.
3. There has been very limited use of magnesium in Soviet
aircraft as compared with equivalent US types.
4. The ratio of steel to aluminum in Soviet aircraft can be
expected to remain high in comparison to US aircraft.
5. The ratios of unskilled to skilled workers and managerial
to production workers are higher in the Soviet aircraft industry
than in the US aircraft industry.
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6. The Soviet labor productivity is lower than the US:
therefore, the Russians require more labor than the US to produce
a given number of aircraft in a stated floor area.
7. Soviet aircraft plants have a higher density of workers
per square foot of floor area than do US aircraft plants.
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APPENDIX A
PLANT STUDIES
The input requirements required by the individual Soviet air-
frame plants to support both current and capacity production are
presented in this appendix. The inputs for capacity have been
based on production estimates projected 3 years in advance of
January 1954.
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b -.6 -U -11-.6 -T
1. Plant PhAmber:
2. Plant Location:
a. Nearest City and Coordinates: Kuybyshev
b. Economic Region: VI
3. Plant Area: 1,790,000 square feet
4. Scale of Effort: 45 percent
5. Production Data:
a. 1953 Production:
Model
Unknown
Airframe Weight
Pounds per Year
(Pounds) Units per Year (including Spares)
Unknown
b. Capacity Production:
Year
1954
1955
1956
Model Units
Unknown
per Year
ANIR weight
pounds
MOT weight
pounds
ANTIS weight
pounds
under 20,000
Unknown
under 20,060
Unknown
under 20,000
Unknown
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Unknown
Pounds per Year
(including Spares)
10,740,000
19,080,000
22,440,000
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6. Input Data:
Production
1953
1954
Capacity
1955
Capacity
1956
Capacity
a. Materials:
S-E-C-R-E-T
Yearly Gross Requirements
- (Metric Tons)
4-) H
03 a)
4-)
CH m
o 0
P4 rPt
0
?
rd
0
H??-?
? H
O o
?H W
4-, M
0
m
r-I
W
01.)
d
0 W
H O
Stainless Steel
and Plastics
175
2,980
28.2
5,160
195
50.2
44.8
185
63.3
311.
5,290
50.2
9,170
346
89.1
79.6
329
112
367
6,240
59.2
lol800
4o8
105
93.8
388
133
b.
Manpower:
Manpower Requirements
(Man-Years)
Production
Total
Direct
Indirect
Skilled
Unskilled
Mana-
gerial
Tech-
nical
1953
10,850
5,425
5,425
3,800
7,050
2,170
1,950
1954 Capacity
23,900
11,950
11,950
- 8,360
15,540
4,780
4,300
1955 Capacity
23,900
11,950
11,950
8,360.
15,540
4,780
4,300
1956 Capacity
23,900
11,950
11,950
-8,360
15,540
4,780
4,300
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c. Electrical Energy:
Source: Kuybyshev Heat and Power Plant,
Alternate Source: Unknown
Production
Electrical Energy Requirements
(Kilowatt-Hours)
1953
16,000,000
1954 Capacity
35,200,000
1955 Capacity
35,200,000
1956 Capacity
35,200,000
d. Fuel and Lubricants:
Fuel Lubricants
Production
Coal
(Metric Tons)
Lube Grease
(Metric Tons)
Lube Oil
(Gallons)
Cutting Oils
1953
27,600
2.52
18,800
_(g,211ons)
6,930
1954 Capacity
49,400
5.58
. 41,700
15,400
1955 Capaci-ty
49,400
5.58
41,700
15,400
1956 Capacity
49,400
5.58
41,700
15,400
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e. Transportation:
S-E-C-R-g-T
Transportation Required
(Metric Tons)
Products Transported
Products Transported to Plant from Plant
Com- Raw
Production Engines ponents Materials
Fuel
Lubri- Spare
cants Aircraft Parts Scrap..
1953
Unknown Unknown
Unknown
27,600
90
Unknown
Un- Un-
known known
1954
Un-
Capacity
Unknown Unknown
8,880
49,400
199.6
Unknown
known 4,010
1955
Un-
Capacity
Unknown Unknown
15,800
49,400
199.6
Unknown
known 7,140
1956
Un-
Capacity
Unkncwn Unknown
18,600
49,400
199.6
Unknown
known 8,410
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1. Plant Number:
S-E-C-R-E-T
2. Plant Location:
a. Nearest City and Coordinates: Kuybyshev
b. Economic Region: VI
3. Plant Area: 1,790,000 square feet
4. Scale of Effort.: 30 percent
5. Production Data:
a. 1953 Production:
Airframe Weight Pounds per Year
Model (Pounds) Units per Year (including Spares)
5,724,000
Tu-4 48,114 108
b. Capacity Production:
Year
Model
Units per Year
Pounds per Year
(including Spares)
194
Tu-4
178
9,300,000
1955
Tu-4
356
18,600,000
1956
Tu-4
424
22,200,000
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?
6. Input Data:
a. Materials:
Production
S-E-C-R-E-T
Yearly Gross Requirements
(Metric Tons)
IL ow-Carbon Steel
1953 70.1 1,230
1954
Capacity 114 2,000
1955
Capacity 228 4,010
1956
Capacity
272 4,780
b. Manpower:
Stainless Steel
Ea
o
H
w
a) a3
P4 Prl 9
P4 -.-1
0 ;-1 CI)
C..) a) a) a)
P4 0
rg X)
PI
gl r0
o a) 0
C.) Z 1-1 14
and Plastics
10.4
2,930
85.7
8.0
2.6
88.2
49.3
18.6
4,770
139
13.1
4.2
143
80.2
37.1
9,540
278
26.2
8.4
287
160
44.3
11,400
332
31.2
10.1
342
191
Manpower Requirements
(Man-Years)
Production
Total
Direct
Indirect
Skilled
1953
7,170
3,585
3,585
2,510
1954 Capacity
23,900
11,950
11,950
8,360
1955 Capacity
23,900
11,950
11,950
8,360
1956 Capacity
23,900
11,950
11,950
8,360
- 56 -
S-E-C-R-E-T
Mana- Tech-
Unskilled gerial nical
4,660
1,430
1,290
15,540
4,780
4,300
15,540
4,780
4,300
15,540
4,780
4,300
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C-R-E-T
c. Electrical Energy:
Source: Kuybyshev Heat and Power Plant,
Alternate Source: Unknown
Production
Electrical Energy Requirements
(Ki1owatt-Hours)
1953
10,600,000
1954 Capacity
35,200,000
1955 Capacity
35,200,000
1956 Capacity
35,200,000
d. Fuel and Lubricants:
Production
Fuel
Lubricants
Coal
(Metric Tons)
Lube Grease
(Metric Timis)
Lube Oil
(Gallons)
Cutting Oils
(Gallons)
1953
27,600
1.68
12,500
4,620
1954 Capacity
49,40o
.5.58
41,700
15,400
1955 Capacity-
49,400
5.58
41,700
15,400
1956 Capacity
49,400
5.58
41,700
15,400
- 57 -
s-E-C -R -E -T
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
e. Transportation:
S-E-C-R-E-T
Transportation Required
(Metric Tons)
Production
Products Transported to Plant
Products Transported
from Plant
Com- Raw
Engines ponents Materials
Fuel
Lubri- Spare
cants Aircraft Parts Scrap
1953
580
502
4,474.3
27,600
59.9
0
208
1,874
1954
Capacity
956
827
7,282.1
49,400
199.6
0
338
31062
1955
Capacity
1,911
1,654
14,324.5
49,400
199..6
0
675
5,884
1956
Capacity
2,230
1,970
170402.6
49,400
199.6
0
806
7,333
-58-
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part- Sanitized Copy Approved forRelease2013/12/12 : CIA-RDP79R01141A000300080002-7
1. Plant Number:
2. Plant Location:
a. Nearest City and Coordinates: Gor'kiy
b. Economic Region: VII
3. Plant Area: 1,337,000 square feet
4. Scale of Effort: 45 percent
5. Production Data:
a. 1953 Production:
50X1
Airframe Weight Pounds per Year
Model (Pounds) Units per Year (including Spares)
MIG-15
or Variant 6065 a/ 605 5,240,000
a. Airframe weight of MIG-15 or variant is assumed to be 6,065
pounds, the average of the MIG-15 and Type 38.
b. Capacity Production:
Year Model
Units per Year
Pounds per Year
(including Spares)
1954 MIG-15
or Variant
1,039
9,000,000
1955 MIG-15
or Variant
1,846
16,000,000
1956 MIG-15
or Variant
2,170
18,800,000
59-
50X1
S-E-C -R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
6. Input Data:
Production
1953
1954
Capacity
1955
Capacity
1956
Capacity
a. Materials:
S-E-C -R-E-T
- - - - -
Yearly Gross Requirements
(.Metric Tons)
IL ow-Carbon Steel
Stainless Steel
H
P
0 0
P4P1
0
0 (1) a)
P4
o
E.) 1-1
114
1,980
18.6
1,760
133
7.9
196
3,400
31.8
3,020
229
13.5
348
6,040
56.6
5,360
406
23.9
409
7,090
66.5
6,300
477
28.1
b. Manpower:
Manpower Requirements
(Man-Years)
Glass and Plastics
16.2 32.1 46.4
27.8 55.1 79.6
49.:q 98.0 142
58.0 115 166
Mana- Tech-
Production Total Direct Indirect Skilled Unskilled gerial nical
1953
8,100
4,050
4,050
2,840
5,260
1,620
1,460
1954 Capacity
17,830
8,915
8,915
6,230
11,600
3,570
3,210
1955 Capacity
17,830
8,915
8,915
6,230
11,600
3,570
3,210
1956 Capacity
17,830
8,915
8,915
6,230
11,600
3,570
3,210
- 60 -
S-E-C-R-E-T
_ _
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C-R-E-T
c. Electrical Energy:
Source: Outside, probably Balakhna Power Station
Alternate Source: City Power Station
Production
Electrical Energy Requirements
(Kilowatt-Hours)
1953
12,000,000
1954 Capacity
26,300,000
1955 Capacity
26,300,000
1956 Capacity
26,300,000
d. Fuel and Lubricants:
Fuel Lubricants
Production
Coal
(Metric Tons)
Lube Grease
(Metric Tons)
Lube Oil
(Gallone).
Cutting Oils
(Gallons)
1953
21,500
1.88
14,000
5,180
1954 Capacity
38,500
4.17
31,200
11,500
1955 Capacity
38,500
4.17
31,200
11,500
1956 Capacity
38,500
4.17
31,200
11,500
- 61 -
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
e. Transportation:
S-E-C-R-E-T
Transportation Required
(Metric Tons)
Production
Products Transported to Plant
Products Transported
from Plant
Com- Raw
Engines ponents Materials
Fuel
Lubri- Spare.
cants Aircraft Parts Scrap
1953
543
103
4,108
21,500
67.1
2,310
708
1,728
1954
Capacity
933
177
7,052.8
38,500
149.2
3,970
1,220
2,973
1955
Capacity
L,660
314
12,523.8
38,500
149.2
7,050
2,180
5,264
1956
Capacity
1,950
369
14,709.6
38,500
149.2
8,290
2,540
6,180
- 62 -
S -E -C -R -E -T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12: CIA-RDP79R01141A000300080002-7
1. Plant Number:
S-E-C-R-E-T
2. Plant Location:
a. Nearest City and Coordinates: Kazan'
b. Economic Region: VI
3. Plant Area: 2,190,000 square feet
4. Scale of Effort: 65 percent
5. Production Data:
a. 1953 Production:
Airframe Weight Pounds per Year
Model (Pounds) Units per Year (including Spares)
Tu-Il- 48,114
b. Capacity Production:
204 10,510,000
Year
Model
Units per Year
Pounds per Year
(including Spares)
1954
Tu-4
341
17,810,000
1955
Tu-4
480
25,100,000
1956
Tu-4
541
28,300,000
- 63 -
S-E-C -R -E -T
? ? ? ? ?
50X1
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
6. Input Data:
a. Materials:
S-E-C-R-E-T
Yearly Gross Requirements
(Metric Tons)
Production
1953
1954
Capacity
1955
Capacity
1956
Capacity
I
rd
O H
O 0
H 0 (I
4-)
4.)(I) 0
......m
0) a)
o,-1 H
U)
o 4-,
it A
11) 1.r4 Ca
M
1?H
cci 4-, P4
W 0
00) a) o ca
r-LI-- 4-)
03
.rd
0
P4 rg
W r0
0 H
d
0 bD P4 0 r0 M
W 0 i 1-1 IZ 0
129
2,260
21.0
5,380
157
14.8
4.8
162
90?5
218
3,840
35.5
9,130
267
25.0
8.1
275
154
307
5,410
50.1
12,900
376
35.3
11.4
387
216
347
6,100
56.5
14,500
424
39.8
12.8
436
211.11.
b. Manpower:
Production
Manpower Requirements
(Man-Years)
Total
Direct
Indirect
Skilled
Unskilled
Mana-
gerial
Tech-
nical
1953
19,000
9,500
9,500
6,650
12,350
3,800
3,420
1954 Capacity
29,200
14,600
14,600
10,200
19,000
5,840
5,260
1955 Capacity
29,200
14,600
14,600
10,200
19,000
5,840
5,260
1956 Capacity
29,200
14,600
14,600
10,200
19,000
5,840
5,260
-E -C -R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C-R-E-T
c. Electrical Energy:
Source: Kazan' Heat and Power Plant,
Alternate Source: Plant may have electric generating equipment
Production
Electrical Energy Requirements
(Kilowatt-Hours)
1953
28,000,000
1954 Capacity
43,100,000
1955 Capacity
43,100,000
1956 Capacity
43,100,000
d. Fuel and Lubricants:
Fuel Lubricants
Coal Lube arease Lube Oil Cutting Oils
Production P
-ro (Metric Tons) (Metric Tons (Gallons) (Gallons)
1953
49,900
4.44
33,200
12,300
1954 Capacity
64,200
6.84
51,000
18,900
1955 Capacity
64,200
6.84
51,000
18,900
1956 Capacity
64,200
6.84
51,000
18,900
- 65 -
S-E-C-R-E-T
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Transportation:
S -E -C -R -E -T
_ _ _ _ _
Transportation Required
(Metric Tons)
Production
Products Transported to Plant
Products Transported
from Plant
Com- Raw
Engines ponents Materials
Fuel
Lubri- Spare
cants Aircraft Parts Scrap
1953
1,096
948
8,221.9
49,900
165.9 0 295 3,457
1954
Capacity
1,832
1,584
13,952.6
64,200
244.8
0
646
5,873
1955
Capacity
2,580
2,230
19,692.8
64,200
244.8
0
911
8,303
1956
Capacity
2,910
2,510
22,160.1
64,200
244.8
0
1,028
9,320
-66-
S -E -C -R -E -T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
41P
1. Plant Number:
S-E-C-R-E-T
2. Plant Location:
a. Nearest City and Coordinates: Moscow
b. Economic Region: VII
3. Plant Area: 1,995,600 square feet
4. Scale of Effort: percent
5. Production Data:
a. 1953 Production:
Airframe Weight Pounds per Year
Model (Pounds) Units per Year (including Spares)
Aircraft Development
b. Capacity Production:
Pounds per Year
Year Model Units per Year (including Spares)
1954 AMPR weight over 20,000
pounds 14,370,000
1955 AMPR weight over 20,000
pounds 24,250,000
1956 AMFR weight over 20,000
pounds 28,130,000
-67-
S-E-C-R-E-T
50X1
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
6. Input Data:
Production
1953
1954
Capacity
1955
Capacity
1956
Capacity
a. Materials:
r-J
a)
a)
h14
S-E-C-R-E-T
Yearly Gross Requirements
(Metric Tons)
b.
Production
Stainless Steel
Glass and Plastics
176 3,100
28.7
7,370 215 20.2
6.5
222
124
297 5,220
48.4
12,400 363 34.1
11.0
374
209
345 61060
56.2
14,400 421 39.6
12.8
434
243
Manpower:
Manpower Requirements
(Man-Years)
Mana-
Tech-
Total
Mrect
Indirect Skilled Unskilled
gerial
nical
1953
12,100
61050
61o5o
4,230
7,870
21420
2,180
1954 Capacity
26,600
13,300
13,300
9,300
17,300
5,320
4,790
1955 Capacity
26,600
13,300
13,300
9,300
17,300
5,320
4,790
1956 Capacity
26,600
13,300
13,300
9,300
17,300
5,320
4,790
- 68 -
S-E-C-R-E-T
_ _ _ _ _ _
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C-R-E-T
Electrical Energy:
Source: Moscow City System
Alternate SouLee: Plant emergency generator
Production
Electrical Energy Requirements
(Kilowatt-Hours)
1953
17,900,000
1954 Capacity
39,300,000
1955 Capacity
39,300,000
1956 Capacity
39,300,000
d. Fuel and Lubricants:
Fuel Lubricants
Production
Coal
(Metric Tons)
Lupe Grease
(Metric Tons)
Lube Oil
(Gallons)
Cutting Oils
(Gallons)
1953
31,100
2.80
20,900
12,300
1954 Capacity
55,900
6.22
46,500
17,200
1955 Capacity
55,900
6.22
46,500
17,200
1956 Capacity
55,900
6.22
46,500
17,200
- 69 -
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
e. Transportation:
SE-C-R-E-T
Transportation Required
(Metric Tons)
Production
Products Transported to Plant
Products Transported
from Plant
Com- Raw
Engines ponents Materials
Fuel
Lubri- Spare
cants Aircraft Parts Scrap
1953
31,100
115.8
1954
Un-
Capacity
Unknown Unknown 11,262.4
55,900
223.2 Unknown
known 4,742
1955
Un-
Capacity
Unknown Unknown 181965.5
55,900
223.2 Unknown
known 7,957
1956
Un-
Capacity
Unknown Unknown 221011.6
55,900
223.2 Unknown
known 9,252
- 70 -
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C -R-E-T
1. Plant Number:
2. Plant Location:
a. Nearest City and Coordinates: Moscow
b. Economic Region: VII
3. Plant Area: 1,230,000 square feet
4. Scale of Effort: 45 percent
5. Production Data:
a. 1953 Production:
Airframe Weight Pounds per Year
Model (Pounds) Units per Year (including Spares)
11-28 16,840 360 61648,000
b. Capacity Production:
Year
Model
Units per Year
Pounds per Year
(including Spares)
1954
11-28
484
8,860l000
1955
11-28
. 817
14,950,000
1956
11-28
948
17,350,000
- 71 -
S-E-C-R-E-T
50X1
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
6. Input Data:
a. Materials:
S-E-C-R-E-T
Yearly Gross Requirements
(Metric Tons)
ri!1
1 H? '
O H
.--1 0 0 -.. .
;..1 -,--1 a) . M
W -I-3
-i-) H -P Ca
CCI 0 0 H H
0 M
,
-P -C1)
cH CO o
o H H 0
N P4
Pi MI
M
C.) 0 0 .1-1 0 0
P s-, (1)4.)
8 .)C13 o $.4 m
'3 ..g C...) CU
P4
H o w
P4 w
g
qg ,0
U) m
m
if
_IA- ? o
.4
,o
m
O H
0
It
Production o
and Plastics
1953 126
/954
Capacity 169
1955
Capacity 285
1956
Capacity 331
2,180
20.5
3,800
133
11.8
6.o
187
21.1
2,900
27.3
51060
177
15.7
8.o
249
28.1
4,890
46.1
8,540
298
26.4
13.5
420
47.4
5,680
53.5
9,920
346
30.7
15.7
488
55.1
b. Manpower:
Production
Manpower Requirements
(Man-Years)
Total
Direct
Indirect
Skilled
Unskilled
Mana-
gerial
Tech-
nical
1953
7,450
3,725
3,725
2,610
4,840
1,490
1,340
1954 Capacity
16,400
8,200
8,200
5,740
10,660
3,280
2,950
1955 Capacity
16,400
8,200
8,200
5,740
10,660
3,280
2,950
1956 Capacity
16,400
8,200
8,200
5,740
10,660
3,280
2,950
- 72 -
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C -R-E-T
c. Electrical Energy:
Source: Moscow City System
Alternate Source: Plant power station
Production
Electrical Energy Requirements
(Kilowatt-HOurs)
1953
11,000,000
1954 Capacity
24,200,000
1955 Capacity
24,200,000
1956 Capacity
24,200,000
d. Fuel and Lubricants:
Fuel_ Lubricants
Production
Coal
(Metric Tons)
Lube Grease
Metric Tons)
Lube Oil
(Gallons)
Cutting Oils
(Gallons)
1953
19,200
1.73
12,900
4,770
1954 Capacity
34,400
. 3.84
28,700
10,660
1955 Capacity
34,400
3.84
28,700
10,660
1956 Capacity
34,400
3.84
28,700
10,660
-73-
S-E -C -R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
e. Transportation:
S-E-C -R-E-T
_ _ _ _ _
Transportation Required
(Metric Tons)
Production
Products Transported to Plant
Products Transported
from Plant
Com- Raw
Engines ponents Materials
Fuel
Lubri- Spare
cants Aircraft Parts Scrap
1953
646
461
6,485.4
19,200
61.8
o
267
3,468,
1954
_Capacity
869
620
8,634.1
28,700
137.8
0
320
4,614
1955
Capacity
1,470
1,050
14,566.4
28,700
137.8
0
540
7,786
1956
Capacity
1,713
1,210
16,920.0
28,700
137.8
0
630
9,050
- 74 -
S-E -C -R-E-T
IDeclassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
1. Plant Number:
S-E-C-R-E-T
2. Plant Location:
a., Nearest City and Coordinates: Tbilisi
b. Economic Region: V
3, Plant Area,: 1,600,000 square feet
4. Scale of Effort: 35 percent
5. Production Data:
a. 1953 Production:
50X1
Airframe Weight Pounds per Year
Model (Pounds) Units per Year (including Spares)
MIG-15
or Variant 6,065 571 4,370,000
b. Capacity Production:
Year Model
Units per Year
Pounds per Year
(including Spares)
1954 MIG-15
or Variant
976
7,470,000
1955 MIG-15
or Variant
2,120
16,210,000
1956 MIG-15
or Variant
. 2,560
19,620,000
-75-
S-E-C-R-E-T
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
6. Input Data:
a. Materials:
S-E-C-R-E-T
Yearly Gross Requirements
(Metric Tons)
,'t
0
OH
H 0 0
H 0 m
O -P >?
-P H -P M 0
d 0 0 H H
0 m
...., r.o
()
Cl)M
CHll0
I
CO
S-4 En
W
0
O 0
P +3 W
(1) -H W
4 r0 d
M
al
1d p4
P4
Cl)M 0 $-4 M $.4
o00) o w
g .0 P4
P4 0
01 g ro
ro
Production 1:11__ 0 0 0
__IA__ 0
6.5
26.7 38.6
Glass and Plastics
1953 13.5
95.0
1,650
15.4
1,460
111
/954
Capacity
163
2,820
26.4
2,510
190
11.2
23.0
45.8
66.1
1955
Capacity
353
6,120
57.4
5,430
412
24.3
50.0
99.2
143
1956
Capacity
427
7,400
69.4
6,580
516
29.4
60.5
120
174
b. Manpower:
Production
1953
1954 Capacity
1955 Capacity
1956 Capacity
Manpower Requirements
(Man-Years)
Total
Direct
Indirect
Skilled
Unskilled
Mana-
gerial
Tech-
nical
7,460
3,730
3,730
2,610
4,850
1,490
1,340.
21,300
10,650
10,650
7,450
13,850
4,260
3,830
21,300
10,650
10,650
7,450
13,850
4,260
3,830
21,300
10,650
10,650
7,450
13,850
4,260
3,830
- 76 -
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12: CIA-RDP79R01141A000300080002-7
c. Electrical Energy:
Source: Tbilisi Power Plant
Alternate Source: Plant generating system
Production
Electrical Energy Requirements
(Kilowatt-Hours)
1953
'11,000,000
1954 Capacity
31,600,000-
1955 Capacity
31,600,000
1956 Capacity
31,600,000
d. Fuel and Lubricants:
Fuel
Lubricants
Production
Coal
(Metric Tons)
Lube Grease
(Metric Tons)
Lube Oil
(Gallons)
Cutting Oils
(Gallons)
1953
11,600
1.75
13,100
4,830
1954 Capacity
20,800
4.99
37,300
13,800
1955 Capacity
20,800,
4.99
37,300
13,800
1956 Capacity
20,800
4.99
37,300
13,800
- 77 -
S-E-C-R-E-T
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Transportation:
S-E -C -R-E-T
_ _ _ _ _
Transportation Required
(Metric Tons)
Production
Products Transported to Plant
Products Transported
from Plant
Com- Raw
Engines ponents Materials
Fuel
Lubri-
cants
Spare
Aircraft Parts Scrap
1953
513
97
3,416.7
11,600
62.7
2,180
413
1,445
1954
Capacity
876
166
5,855.5
20,800
179.0
3,730
703
2,468
1955
Capacity
1,900
360
12,318.1
20,800
179.0
8,100
1,520
4,963
1956
Capacity
2,300
435
15,376.3
20,800
179.0
9,780
1, 86o
6,476
-78-
S -E -C -R -E -T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E -C -R-E-T
1. Plant Number:
2. Plant Location:
a. Nearest City and Coordinates: Irkutsk
b. Economic Region: XI
3. Plant Area: 1,5001000 square feet
4. Scale of Effort: 40 percent ?
5. Production Data:
a. 1953 Production:
Airframe Weight Pounds per Year
Model (Pounds) Units per Year (including Spares)
TYPP 35 17,000 384 7,200,000
b. Capacity Production:
Year Model Units per Year
Pounds per Year
(including Spares)
1954
Type 35
584
10,800,000
1955
Type 35
986
18,200,000
1956
Type 35
1,145
21,150,000
-79-
S -E -C -R -E -T
50X1
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
6. Input Data:
Production
1953
/954
Capacity
1955
Capacity
1956
Capacity
a. Materials:
S-E-C-R-E-T
Yearly Gross Requirements
(Metric Tons)
137
206
347
403
Stainless Steel
Cl)
0
H
0
$4 0
0 0
PIP:1
M
P4
0 ;.4 M
C.) CD a) o
P1 g
1 ,0
P4 rIP
o o 0
0
and Plastics
2,360
22.2
4,120
144
12.7
6.5
202
22.9
3,540
33.3
6,180
216
19.1
9.8
304
34.3
5,960
56.2
10,400
363
32.2
16.5
512
57.8
6,920
65.2
12,100
422
37.4
19.2
594
67.2
b. Manpower:
Production
_
1953
1954 Capacity
1955 Capacity
1956 Capacity
Manpower Requirements
(Man-Years)
Total
Direct
Indirect
Skilled
Unskilled
Mana-
gerial
Tech-
nical
8,000
41000
4l000
21800
5,200
1,600
11440
20,000
10,000
10,000
7,000
13,000
4,000
3,600
20,000
10,000
10,000
7,000
13,000
41000
3,600
20,000
10,000
10,000
7,000
13,000
41000
3,600
- 8o -
S-E-C-R-E-T
?IIMM ?????
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C -R-E-T
c. Electrical Energy:
Source: Thermo-electric generator located Within plant area
Alternate Source: Auxiliary plant power plant
Production
Electrical Energy Requirements
(Kilowatt-gours)
1953
11,800,000
1954 Capacity
29,500,000
1955 Capacity
29,500 000
1956 Capacity
29,500,000
d. Fuel and Lubricants:
Production
Fuel
Lubricants
Coal
(Metric Tons)
Lube Grease
(Metric Tons
Lube Oil
(Gallons)
Cutting Oils
(Gallons)
1953
22,200
1.87
14,000
5,160
1954 Capacity
39,900
4.69
35,000
12,900
1955 Capacity
39,900
4.69
35,000
12,900
1956 Capacity
39,900
4.69
35,000
12,900
- 81 -
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
e. Transportation:
S-E-C -R-E-T
? ? ? ? ?
Transportation Required
(Metric Tons)
Production
Products Transported to Plant
Products Transported
from Plant
Com- Raw
Engines ponents Materials
Fuel
Lubri- Spare
cants Aircraft Parts Scrap
1953
690
758
7,027.3
22,200
67.1 0 305 3,762
1954
Capacity
1,050
11150
10;542.5
39,900
167.7
0
390
5,643
1955
Capacity
1,770
1,930
17,744.7
39,900
167.7
0
655
9,490
1256
Capacity
2,060
2,260
201628.0
39,900
167.7
0
765
11,033
-82 -
S-E-C -R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
1. Plant Number:
S-E-C-R-E-T
2. Plant Location:
a. Nearest City and Coordinates: Chkalov
b. Economic Region: VIII
3. Plant Area: 381,000 square feet
4. Scale of Effort: 45 percent
5. Production Data:
a. 1953 Production:
Airframe Weight Pounds per Year
Model (Pounds) Units per Year (including Spares)
Type 24 6,300 192 1,500,000
b. Capacity Production:
Year Model Units per Year
Pounds per Year
(including Spares)
1954
Type 24
261
2,058,000
1955
Type 24
464
3,660,000
1956
Type 24
546
4,295,000
-83-
S-E -C -R-E-T
50X1
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
6. Input Data:
Production
a. Materials:
a)
Ri P:1
fil H
N
s
rd
d
OH
0 a)
-r-t a)
4-)
4-)
H
4-)Cl)
fa)
0
0
Cl)
A-)
, Er)
0,1
0
CO
a)
H,--I
0
1:1)
0
(1) -H
g4'
C3
co 4-)
CO
0
S-E-C-R-E-T
Yearly Gross Requirements
(Metric Tons)
Cl)
0
iD

9
0(13
H CO
c.) a) a) a)
H 0
OD to
0 Pi
Pi 0
g
rd
cd
ro
ra
Ci)
0
_a__ -H o
o Z 1-1 14
o
1953 18.4
1954
Capacity
1955
Capacity
1956
Capacity
25.2
44.8
52.6
312
2.9
796
19.7
0
2.3
427
4.0
1,090
27.1
o
3.2
760
7.1
1,940
48.1
o
5.6
892
8.4
2,280
56.3
o
6.6
b. Manpower:
Manpower Requirements
(Man-Years)
Glass and Plastics
4.4 6.7
6.1 9.1
10.8. 16.3
12.7 19.1
Mana- Tech-
Production Total Direct Indirect Skilled Unskilled gerial nical
1953
2,290
1,145
1,145
800
1,490
1i-58
412
1954 Capacity
5,080
2,540
2,540
1,780
3,300
1,020
914
1955 Capacity
5,080
2,540
2,540
1,780 .
3,300
1,020
914
1956 Capacity
5,080
2,540
2,540
1,780
3,300
1,020
914
- 84 -
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C -R-E-T
c. Electrical Energy:
Source: Chkalov Power Plant, TETS "Krasny Mayak"
Alternate Source: Auxiliary pia:it power plant
Production
Electrical Energy Requirements
(Kilowatt-Hours)
1953
3,410,000
1954 Capacity
71500,000
1955 Capacity
7,500,000
1956 Capacity
7,500,000
d. Fuel and Lubricants:
Fuel Lubricants
Production
Coal
(Metric Tons)
Lube Grease
(Metric Tons)
Lube Oil
(Gallons)
Cutting Oils
(Gallons)
1953
6,48o
0.53
4,0oo
1,43o
1954 Capacity
10,600
1.19
8,880
3,280
1955 Capacity
10,600
1.19
8,880
3,280
1956 Capacity
10,600
1.19
8,880
3,280
-85-
S-E -C -R -E-T
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
e. Transportation:
S-E-C-R-E-T
Transportation Required
(Metric Tons)
Products Transported to Plant
Products Transported
from Plant
Com- Raw
Production Engines ponents Materials
Fuel
Lubri- Spare
cants Aircraft Parts Scrap
1953
o
o
1,162.4
6,480
16.1
549.
132
482
1954
Capacity
0
0
1,591.7
10,600
42.5
746
288
658
1955
Capacity
0
0
2,832.7
10,600
42.5
1,330
334
1,173
1956
Capacity
0
0
3,327.9
lo1600
42.5
1,560
388
1,380
- 86 -
S-E-C -R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
1. Plant Number:
S-E-C-R-E-T
2. Plant Location:
a. Nearest City and Coordinates: Taganrog
b. EcOnanic Region:
3. Plant Area: 1,262,000 square feet
.4. Scale of Effort: 45 percent
5. Production Data:
a. 1953 Production:
Airframe Weight
Model (Pounds)
Units per Year
50X1
Pounds per Year
(including Spares)
Type 33
5,040
133
843,000
Type 34
20,500
44
1,127,000
Li-2
13,372
135
2,318,000
b. Capacity Production:
Year
Model
Pounds per Year
(including Spares)
1954
AMPR weight
under 20,000
pounds
8,520,000
1955
AMER weight
under 20,000
pounds
15,140,000
1956
AMTR weight
under 20,000
pounds
17,780,000
-87-
S-E-C -R-E-T
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
6. Input Data:
a. Materials:
Production
S-E-C-R-E-T
Yearly Gross Requirements
(Metric Tons)
IL ow-Carbon Steel
1953 40 759
1954
Capacity 139 2,370
1955
Capacity 247 4,200
1956
Capacity 290 4,940
b. Manpower:
a)
3-1 m
a) cd
9
failog
0 P m
OG) 0 a)
P4 0 rd X)
014 g) a3 ,0
o m 0
c.) Z 1-1 14
and Plastics
6.4
2,009
40.2
12.6
7.7
66.2
34.3
22.4
4,100
155
39.8
35.6
147
50.2
39.8
7,280
275
70.8
63.2
261
89.3
46.8
8,550
323
83.1
74.2
306
105
Manpower Requirements
(Man-Years)
Production
Total
Direct
Indirect
Skilled
Unskilled
Mana-
gerial
1953
6,060
3,030
3,030
2,120
3,940
1,210
1954 Capacity
16,820
8,410
8,410
5,890
10,930
3,360
1955 Capacity
16,820
8,410
8,410
5,890
10,930
3,360
1956 Capacity
16,820
8,410
8,410
5,890
10,930
3,360
- 88 -
S-E-C-R-E-T
Tech-
nical
1,090
3,030
3,030
3,030
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C-R-E-T
c. Electrical Energy:
Source: Outside, probably Taganrog City System
Alternate Source: Plant power station
Electrical Energy Requirements
Production (Kilowatt-Hours)
1953
8,950,000
1954 Capacity
24,800,000
1955 Capacity
24,8400,000
1956 Capacity
241800,000
d. Fuel and Lubricants:
Fuel Lubricants
Production
Coal
(Metric Tons)
Lube Grease
(Metric Tons)
Lube Oil
(Gallons)
Cutting OilE
(Gallons)
1953
11,600
1.40
10,500
3,880
1954 Capacity
26,400
3.94
291400
10,980
1955 Capacity-
261400
3.94
291400
10,980
1956 Capacity
26,1400
3.94
291400
10,980
-89-
S-E-C -R-E -T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
e. Transportation:
S-E-C-R-E-T
Transportation Required
(Metric Tons)
Production
Products Transported to Plant
Products Transported
from Plant
Com- Raw
Engines ponents Materials
Fuel
Lubri- Spare
cants Aircraft Parts Scrap
1953
295 274 2,975.4
11,600
,
50.3 0 413 1,030
1954
Un-
Capacity
Unknown Unknown 7,059.0
26,400
141.3 Unknown
known 3,196
1955
Un-
Capacity
Unknown Unknown 12,526.1
26,400
141.3 Unknown
known 5,656
1956
Un-
Capacity
Unknown Unknown 14,718.1
26,400
141.3 Unknown
known 6,653
- 90 -
S-E-C -R-E -T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
a
a
1. Plant Number:
S -E -C -R -E -T
2. Plant Location:
a. Nearest City and Coordinates: Voronezh
b. Economic Region: VII
Plant Area: 1,888,400 square feet
4. Scale of Effort: 45 percent
5. Production Data:
a. 1953 Production:
Airframe Weight Pounds per Year
Model (Pounds) Units per Year (including Spares)
11-28 16,84o
b. Capacity Production:
372 6,792,000
Year
Model
Units per Year
Pounds per Year
(including Spares)
1954
11-28
743
13,600,000
1955
11-28
1,253
22,930,000
1956
11-28
1,453
26,600,000
- 91 -
S-E-C-R-E-T
50X1
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
6. Input Data:
Production
1953
1954
Capacity
1955
Capacity
1956
Capacity
a. Materials:
S-E-C-R-E-T
Yearly Gross Requirements
(Metric Tons)
IL ow-Carbon Steel
rci-i
0
H----
O H
O a)
-I-4 (1) Ul
-P
4-3 En 0
O H
--- u)
Z CO
0
f jr ,-i U)
a.)
? +)
Ca N
P
(r)c P:1
P4 ?r-I
0
Ea P
cU o3
O ? CIO
Pc
Pc 0
a)
ry3 ,0
a)
,0
0
O a)
Glass and Plastics
129
2,220
21.0
3,880
136
12.0
6.2
191
21.6
259
4,450
42.0
7,780
271
24.1
12.3
383
43.2
437
7,510
70.8
13,100
458
40.6
20.8
645
72.8
507
8,710
82.0
15,200
531
47.1
24.1
748
84.4
b. Manpower:
Manpower Requirements
(Man-Years)
Production
Total
Direct
Indirect
Skilled
Unskilled
Mana-
gerial
Tech-
nical
1953
11,450
5,725
5,725
3,990
7,460
2,290
2,060
1954 Capacity
25,200
12,600
12,600
8,820
16,380
5,040
4,540
1955 Capacity
25,200
12,600
12,600
8,820
16,380
5,040
4,540
1956 Capacity
25,200
12,600
12,600
8,820
16,380
5,040
4,540
-.92 -
S-E-C -R -E-T
_ _ _ _ _
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C -R-E-T
C. Electrical Energy:
Source: Voronezh Thermal Power Plant
Alternate Source: Unknown
Production
Electrical Energy Requirements
(Kilowatt-Hours)
1953
16,900,000
1954 Capacity
37,200,000
1955 Capacity
37,200,000
1956 Capacity
37,200,000
d. Fuel and Lubricants:
Production
Lubricants
Coal
(Metric Tons)
Lube Grease
(Metric Tons)
Lube Oil
(Gallons)
Cutting Oils
(Gallons)
1953
25,900
2.65
19,800
7,340
1954 Capacity
46,500
5.89
44,000
16,300
1955 Capacity
46,500
5.89
44,000
16,300
1956 Capacity
46,500
5.89
44,000
16,300
- 93 -
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
e. Transportation:
S-E-C-R-E-T
Transportation Required
(Metric Tons)
Production
Products Transported to Plant
Products Transported
from Plant
Com- Raw
Engines ponents Materials
Fuel
Lubri- Spare
cants Aircraft Parts Scrap
1953
668
476
6,616.8
25,900
60.9
0
240
3,537
1954
Capacity
1,335
951
13,264.6
46,500
210.9
0
495
7,095
1955
Capacity
2,250 .
1,600
22,355.0
46,500
210.9
0
830
11,955
1956
Capacity
2,610
11860
25,933.6
46,500
210.9
0
970
13,874
-94-
S -E -C -R -E -T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
1. Plant Number:
S-E-C-R-E-T
2. Plant Location:
a. Nearest City and Coordinates: Moscow
b. Economic Region: VII
3, Plant Area: 680,000 square feet
4. Scale of Effort: 45 percent
5. Production Data:
a. 1953 Production:
Airframe Weight Pounds per Year
Model (Pounds) Units per Year (including Spares)
Experimental Work and
Aircraft Parts
b. Capacity Production:
Pounds per Year
Year Model (including Spares)
1954 AMPR weight under 20,000
pounds 4,5901000
1955 AMPR weight under 20,000
pounds - 8,160,000
1956 AMPR weight under 20,000
pounds 9,588,000
-95-
S-E-C-R-E-T
50X1
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
6. Input Data:
Production
1953
1954
Capacity
1955
Capacity
1956
Capacity
a. Materials:
S-E-C-R-E-T
Yearly Gross Requirements
(Metric Tons)
4)
0
1
OH
O P
P H P IM
W 0 0
Z 0 M
P -U)
CH W W
O HH
O 0 0
0 0
P4 ro P W
P FA
W M P
M
C.)
0
bo
0
b.
Production
Stainless Steel
U)
o
W
P (j)
ci) 05
Pi P:1
1
Pi
O4 u)
O W
0 rd w
X)
Pi
0 a) 0
0 Z 14 (4
Glass and Plastics
75 1,270
12.1
2,210 83.3 21.4
19.2
79.1
27.1
133 2,270
21.5
3,920 148 38.1
34.0
141
48.1
157 2,660
25.2
4,610 174 44.8
40.0
165
56.6
Manpower:
Manpower Requirements
(Man-Years)
Mana-
Tech-
Total
Direct
Indirect Skilled Unskilled
gerial
nical
1953
4,120
2,060
2,060
14J4-0
2,680
824
742
1954 Capacity
9,070
4,535
4,535
3,170
5,900
1,810
1,630
1955 Capacity
9,070
4,535
4,535
3,170
5,900
1,810
1,630
1956 Capacity
9,070
4,535
4,535
3,170
5,900
1,810
1,630
- 96 -
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E=C-R-E-T
c. Electrical Energy:
Source: Probably Moskva Hydro Power Plant Tushino
Alternate Source: Plant emergency generator
Electrical Energy Requirements
Production (Kilowatt-Hours)
1953
6,o8o,000
1954 Capacity
13,400,000
1955 Capacity
13,400,000
1956 Capacity
13,400,000
d. Fuel and Lubricants:
Fuel Lubricants
Production
Coal
(Metric Tons)
Lube Grease
(Metric Tons)
Lube Oil
(Gallons)
?
Cutting Oils
(Gallons)
1953
10,600
0.95
71110
2,640
1954 Capacity
19,000
2.12
15,800
5,860
1955 Capacity
19,000
2.12
15,800
5,860
1956 Capacity
19,000
2.12
15,800
5,860
-97-
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
e. Transportation:
S-E-C-R-E-T
Transportation Required
(Metric Tons)
Production
Products Transported to Plant
Products Transported
from Plant
Com- Raw
Engines ponents Materials
Fuel
Lubri- Spare
cants Aircraft Parts Scrap
1953
Unknown Unknown
Unknown
10,600
34.1
Unknown
Un- Un-
known known
1954
Capacity
Unknown Unknown
3,797.2
19,000
75.7
Unknown
Un- 1,715
known
1955
Capacity
Unknown Unknown
6,753.7
19,000
75.7
Unknown
Un- 3,053
known
1956
Capacity
Unknown Unknown
7,932.6
19,000
75.7
Unknown
Un- 3,583
known
-98-
S -E -C -R -E -T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
?
1. Plant Number:
S-E-C-R-E-T
2. Plant Location:
a. Nearest City and Coordinates:
b. Economic Region: X
1,320,000 square feet
3. Plant Area:
4. Scale of Effort: 35 percent
5. Production Data:
a. 1953 Production:
Tashkent
Airframe Weight Pounds per Year
Model (Pounds) Units per Year (including Spares)
11-12 16,000 70 1,4o6,000
b. Capacity Production:
Year
Model
Units per Year
Pounds per Year
(including Spares)
1954
11-12
172
3,450,000
1955
11-12
347
6,952,0oc
1956
11-12
772
15,450,000
- 99 -
s-E-C -R -E -T
50X1
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
6. Input Data:
a. Materials:
Type of Material
Production
1953
S-E-C-R-E-T
Yearly Gross Requirements
(Metric Tons)
H .? ..,
OH
? W
?H (1) Cl)
-1-)
H
W 0 H H
(1) m
.1_) ?Cl)
W
Zi 1:) $4 M
W
,0 4-7 W 1004 IA
M
O W ,--1 W d
W
;-4 VI -1-.)
m N 0
p4
co
P4
Pi W
0 rid
c...)
0 w
10,3 40
_IA_
O Fil_
0
0
i-1
0
14
0
16.0 271 2.6 868 23.6 14.0
1954
Capacity 39.1 664 6.3 2,130 57.9 34.4
1955
Capacity 78.8 1,340 12.6 4,290 117 69.4
1956
Capacity 175 2,970 28.0 9,540 259 154
b. Manpower:
Manpower Requirements
(Man-Years)
Glass and Plastics
16.0
31.3
8.3
39.1
76.7
20.3
78.8
154
41.0
175
344
91.2
Production Total Direct Indirect
1953
6116o
3,080
3,080
1954 Capacity
17,600
8,800
8,800
1955 Capacity
17,600
81800
81800
1956 Capacity
17,600
8,800
8,800
S-E-C-R-E-T
Skilled
Unskilled
Mana-
gerial
Tech-
nical
21160
4l000
1,230
1,110
6,160
11,440
3,520
3,170
6,160
11,440
3,520
3,170
6,160
11,440
3,520
3,170
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C-R-E-T
c. Electrical Energy:
Source: Tashkent City ipoWer Supply
Alternate Source: Plant A has auxiliary power plant
Electrical Energy Requirements
Production (Kilowatt-Hours)
1953
9,100,000
1954 Capacity
26,000,000
1955 Capacity
26,000,000
1956 Capacity
26,000,000
d. Fuel and Lubricants:
Production
Fuel
Lubricants
Coal
(Metric Tons)
Lube Grease
Metric Tons)
Lube Oil
(Gallons)
Cutting Oils
(Gallons)
1953
9,570
1.44
10,800
3,990
1954 Capacity
17,100
4.12
30,800
11,400
1955 Capacity
17,100
4.12
30,800
11,400
1956 Capacity
17,100
4.12
30,806
11,400
101 -
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C-R-E-T
?
e. Transportation:
Transportation Required
(Metric Tons)
Production
Products Transported to Plant
Products Transported
from Plant
Com- Raw
Engines ponents Materials
Fuel
Lubri- Spare
cants Aircraft Parts Scrap
1953
126
102
1,250.8
9,570
51.7
0
130
610
1954
Capacity,
309
250
3,067.8
17,100
147.7
0
318
1,500
1955
Capacity
623
505
6,181.6
17,100
147.7
0
635
3,027
1956
Capacity
1,387
1,030
13,736.2
17,100
147.7
0
1,410
6,715
- 102 -
S-E-C-R-E-T
_ _ _ _ _
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
1. Plant Number:
S-E-C-R-E-T
2. Plant Location: ?
a. Nearest City and Coordinates: Ulan-Ude
b. Economic Region: XI
3. Plant Area: 373,311 square feet
Is., Scale of Effort: 45 percent
5. Production Data:
a. 1953 Production:
Airframe. Weight Pounds per Year
Model (Pounds)
MIG-15
or Variant
Units per Year? (including Spares)
6,065 145 1,110,000
b. Capacity Production:
Year Model
Units per Year
Pounds per Year
(including Spares)
1954 MIG-15
or Variant
293
2,240,000
1955 MIG-15
or Variant
522
3,981,000
1956 MIG-15
or Variant
612
4,68o,000
?
50X1
50X1
- 103 -
S-E-C -R-E-T
_ _ _ _ _
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
6. Input Data:
Production
a. Materials:
S-E-CrR-E-T
Yearly Gross Requirements
(Metric Tons)
IL ow-Carbon Steel
r(!i
H
? H
O a)
W
0
rn
HH
a) 0
4)?3
? 4-)
4i
.1)
Stainless Steel
p4
o
CU
z
,0
G4
F34 0
Glass and Plastics
1953 '
24.1 418
3.9
372 28.2 1.7
3.4
6.8
9.8
1954
Capacity
48.8 846
7.9
751 56.9 3.4
6.9
13.7
19.8
1955
Capacity
86.7 1,500
14.1
1,330 101 6.0
12.3
24.4
35.2
1956
Capacity
102 1,770
16.6
1,570 119 7.0
14.4
28.7
41.4
b. Manpower:
Manpower Requirements
(Man-Years)
Mana-
Tech-
Production
Total
Direct
Indirect Skilled Unskilled
gerial
nical
1953
2,240
1,120
1,120
780
1,460
448
403
1954 Capacity
4,980
2,490
2,490
1,740
3,240
996
896
1955 Capacity
4,980
2,490
2,490
1,740
3,240
996
896
1956 Capacity
4,980
2,490
2,490
1,740
3,240
996
- 104 -
S -E -C -R-E-T
(
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7 ,
4
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C-R-E-T
c. Electrical Energy:
Source:. Ulan-Ude Municipal Power Plant
Alternate Source:
Thermo-electric plant within plant area
Production
Electrical Energy Requirements
(Kilowatt-Hours)
1953
3,340,000
1954 Capacity
7,350,000
1955 Capacity
7,350,000
1956 Capacity
7,350,000
d. Fuel and Lubricants:
Production
Fuel
Lubricants
Coal
(Metric Tons)
Lube Grease
(Metric Tons)
Lube Oil
(Gallons)
Cutting Oils
(Gallons)
1953
5,530
0.52
3,920
1,450
1954 Capacity
9,930
1.17
8,700
3,220
1955 Capacity
9,930
1.17
. 8,700
3,220
1956 Capacity
9,930
1.17
8,700
3,220
- 105
S-E-C
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
e. Transportation:
S-E-C -R-E-T
Transportation Required
(Metric Tons)
Production
Products Transported to Plant
Products Transported
from Plant
Com- Raw
Engines ponents Materials
Fuel
Lubri- Spare'
cants Aircraft Parts Scrap
1953
129
25
867.9
5,530
18.8
554
105
365
1954
Capacity
260
50
1,754.4
9,930
41.7
1,120
209
738
1955
Capacity
464
89
3,109.7
9,930
41.7
1,990
367
1,294
1956
Capacity
544
104
3,669.1
9,930
41.7
2,340
44o
1,547
- 106 -
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
1. Plant Number:
S-E-C-R-E-T
2. Plant Location:
. Nearest City and Coordinates: Semenovka
b. Economic Region: XII
3. Plant Area: 275,000 square feet
4. Scale of Effort: 28 percent
5. Production Data:
a. 1953 Production:
Airframe Weight Pounds per Year
Model (Pounds) Units per Year (including Spares)
Yak-18 850 708 749,000
b. Capacity Production:
Year Model Units per Year
Pounds per Year
(including Spares)
1954
Yak-18
1,210
11285/000
1955
Yak-18
2/620
21784,000
1956
Yak-18
3,170
3,370,000
- 107 -
S-E-C-R-E-T
50X1
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
6. Input Data:
Production
1953
1954
Capacity
1955
Capacity
1956
Capacity
a. Materials:
S-E-C-R-E-T
Yearly Gross Requirements
(Metric Tons)
rd
0
H .---.
OH
o o
?H O) Cl)
-1-)
H .4-) cf) 0
O ? (1)
Ha) 0
Cl) 0
HH 0
0 0 P m
P tr) -p
N P4
P4 Gcl
?P-4
o a) .1-1 a) d
,r) 4.3 cd
ca co 0 P w P
0 0 0
P4 0
0 rd
ai -0
ra
a)
C.)
H 0
0 W P4
O 0
i a) 0
_d__ ?H 0 a a
Glass and Plastics
11.5
197
1.8
360
13.9
o
1.6
3.0
4.4
19.4
330
3.1
604
23.4
o
2.6
5.0
7.4
42.9
731
6.8
1,340
51.8
o
5.8
11.0
_ 16.4
52.0
885
8.3
1,620
62.7
o
7.0
13.3
19.9
b. Manpower:
Production
1953
1954 Capacity
1955 Capacity
1956 Capacity
Manpower Requirements
(Man-Years)
Total
Direct
Indirect
Skilled
Unskilled
Mana-
gerial
Tech-
nical
1,030
515
515
360
670
206
185
3,670
1,835
1,835
1,280
2,390
734
660
3,670
1,835
1,835
1,280
2,390
734
660
3,670
1,835
1,835
1,280
2,390
734
660
- 108 -
S-E-C -R-E-T
_ _ _ _ _ _
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C-R-E-T
c. Electrical Energy:
Source: City Power Plant
Alternate Source:
Unknown
Production
Electrical Energy Requirements
(Kilowatt-Hours)
1953
1,520,000
1954 Capacity
5,410,000
1955 Capacity
5,410,000
1956 Capacity
5,410,000
d. Fuel and Lubricants:
Production
Fuel
Lubricants
Coal
(Metric Tons)
Lube Grease
(Metric Tons)
lube Oil
(Gallons)
Cutting Oils
(Gallons)
1953
3,200
0.24
1,790
664
1954 Capacity
5,750
0.85
6,410
2,370
1955 Capacity
5,750
0.85
6,410
2,370
1956 Capacity
5,750
0.85
6,410
2,370
- 109 -
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
e. Transportation:
S-E-C-R-E-T
Transportation Required
(Metric Tons)
Production
Products Transported to Plant
Products Transported
from Plant
Com- Raw
Engines ponents Materials
Fuel
Lubri- Spare
cants Aircraft Parts Scrap
1953
138
101
593.2
3,200
8.5
512
67
253
1954
Capacity
235
173
994.9
5,750
30.7
876
116
412
1955
Capacity
510
375
'
2,205.7
5,750
30.7
1,900
253
943
1956
Capacity
617
453
2,668.2
5,750
30.7
2,300
307
1,139
- 110
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C-R-E-T
?
1. Plant Number:
2. Plant Location:
a. Nearest City and Coordinates: Komsomol'sk
b. Economic Region: VII
3. Plant Area: 1,540,000 square feet
4. Scale of Effort: 45 percent
5. Production Data:
a. 1953 Production:
50X1
Airframe Weight Pounds per Year
Model (Pounds) Units per Year (includi,ng Spares)
MIG-15
or Variant
6,065 632 4,840,000
b. Capacity Production:
Pounds per Year
Year Model Units per Year (including Spares)
1954 MIG-15
or Variant 1,087 8,320,000
1955 MIG-15
or Variant 1,935 14,790,000
1956 MIG-15
or Variant 2,270 17,355,000
S-E-C-R-E-T
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
6. Input Data:
Production
1953
1954
Capacity
1955
Capacity
1956
Capacity
a. Materials:
Type of Material
S-E-C-R-E-T
Yearly Gross Requirements
(Metric Tons)
'Stainless Steel
106
1,830
17.2
1,630
181
3,140
29.4
2,790
322
5,580
52.3
4,960
378
6,550
61.4
5,820
b. Manpower:
co
0
ri
0
f-i En
a) cd
9
p" x1
cli 4-1
O4 CO ..1
00) a) a)
P4 0 rci do
P4
%? al r0
0 (1) 0
0 Z i-1 M
123
7.3
15.0
211
12.5
25.7
376
22.1
45.6
441
26.0
53.6
Manpower Requirements
(Man-Years)
Glass and Plastics
29.7 42.9
51.0 73.6
90.6 131
106 154
Mana- Tech-
Production Total Direct Indirect Skilled Unskilled gerial nical
1953
9,220
4,610
4,610
3,220
6,000
1,840
1,660
1954 Capacity
20,500
10,250
10,250
7,170
13,330
4,100
3,690
1955 Capacity
20,500
10,250
10,250
7,170
13,330
4,100
3,690
1956 Capacity
20,500
10,250
10,250
7,170
13,330
4,100
3,690
-112-
S-E-C-R-E-T
_ _ _ _ _
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C-R-E-T
c. Electrical Energy:
Source: Probably outside source
Alternate Source: Unknown
Electrical Energy Requirements
Production (Kilowatt-Hours)
1953 13,800,000
1954 Capacity 30,300,000
1955 Capacity 30,300,000
1956 Capacity 30,300,000
d. Fuel and Lubricants:
Fuel Lubricants
Coal Lube Grease Lube Oil Cutting Oils
Production (Metric Tons) (Metric Tons) .(Gallons) (Gallops)
1953
30,200
2.17
16,200
5,990
1954 Capacity
54,000
4.81
35,900
13,300
1955 Capacity
54,000
4.81
35,900
13,300
1956 Capacity
54,000
4.81
35,900
13,00
- 113 -
S-E-C-R-E-T
.
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
e. Transportation:
S-E-C-R-E-T
????? 'mom OM* amm
Transportation Required
(Metric Tons)
Production
Products Transported to Plant
Products Transported
from Plant
Com- Raw
Engines ponents Materials
Fuel
Lubri- Spare
cants Aircraft Parts Scrap
1953
586
107
3,801.1
30,000
77.6
2,410
458
1,598
1954
Capacity
976
185
6,324.3
54,000
167.8
4,150
784
2,551
1955
Capacity
1,740
329
11,579.6
54,000
167.8
7,390
1,384
4,875
1956
Capacity
2,040
386
13,590
54,000
167.8
8,670
1,630
5,715
- 114 -
S -E -C -R -E -T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
1. Plant Number:
S-E-C-R-E-T
2. Plant Location:
a. Nearest City and Coordinates: Khar'kov
b. Economic Region: III
3. Plant Area: 710,000 square feet
4. Scale of Effort: 45 percent
5. Production Data:
1953 Production:
Airframe Weight Pounds per Year
Model , (Pounds) Units per Year (including Spares)
MIG-15
or Variant
6,065
b. Capacity Production:
252 3,108,000
Year Model
Units per Year
Pounds per Year
(including Spares)
1954 MIG-15
or Variant
795
4,788,00o
1955 MIO-15
or Variant
1,410
8,520,000
1956 MIG-15
or Variant
1,657
10,000,000
115 -
S-E-C-R-E-T
50X1
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7 -
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
6. Input Data:
Production
1953
1954
Capacity
1955
Capacity
1956
Capacity
4-)
0
a. Materials:
S-E-C-R-E-T
Yearly Gross Requirements
(Metric Tons)
Stainless Steel
Cl]
o
i-1
o
d
a) d
PLI P:1
1
P4
0 $.4 Ca S-1
0 a) 0 a)
P4 P
1 r0
P4
Wa) ,PI
o
o Z 1-1 14
Glass and Plastics
67.7
1,170
11,0
1,040
79
. 4.7
9.6
19.0
27.5
104
1,810
16.9
1,600
122
7.2
14.8
29.3
42.3
185
3,210
30.1
2,850
216
12.7
26..2
52.1
75.3
216
3,780
35.4
3,360
254
15.0
30.9
61.3
88.5
b. Manpower:
Manpower Requirements
(Man-Years)
Production
Total
Direct
Indirect
Skilled
Unskilled
Mana-
gerial
Tech-
nical
1953
4 300
2,150.
2,150
1,500
2,800
860
774
1954 Capacity
9,470
4,735
4,735
3,310
6,160
1,890
1,700
1955 Capacity
9,470
4,735
4,735
3,310
6,160
1,890
1,700
1956 Capacity
9,470
4,735
4,735
3,310
6,160
1,890
1,700
- 116 -
S -E -C -R-E-T
_ _ _ _ _
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C-R-E-T
c. Electrical Energy:
Source: Khartkov Heat and Power Plant
Alternate Source:
Possibly plant power plant
Electrical Energy Requirements
Production (Kilowatt-Hours)
1953
6,350,000
1954 Capacity
14,000,000
1955 Capacity
14,000,000
1956 Capacity
14,000,000
d. Fuel and Lubricants:
Krasnozarod
Production
Fuel
Lubricants
Coal
(Metric Tons)
Lube Grease
(Metric Tons)
Lube Oil
(Gallons)
Cutting Oils
(Gallops)
1953
9,110
1.00
7,420
2,750,
1954 Capacity
16,300
2.22 .
16,500
6,120
1955 Capacity-
16,300
2.22
16,500
6,120
1956 Capacity
16,300
2.22
16,500
6,120
- 117 -
S-E-C -R-E-T
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C-R-E-T
Oh
e. Transportation:
Transportation Required
(Metric Tons)
Production
Products Transported to Plant
Products Transported
from Plant
Com- Raw
Engines ponents Materials
Fuel
Lubri- Spare
cants Aircraft Parts Scrap
1953
226
43
2,428.5
9,110
35.6
963
716
1,020
1954
Capacity
714
135
3,746.5
16,300
79.1
3,040
0
1,575
1955
Capacity
1,270
240
6,657.4
16,300
79.1
5,390
0
2,794
1956
Capacity
1,490
282
7,843.1
16,300
79.1
6,330
0
3,307
- 118 -
S-E-C -R -E -T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C -R-E-T
1. Plant Number:
2. Plant Location:
a. Nearest City and Coordinates: Novosibirsk
b. Economic Region: IX
3. Plant Area: 2,100,000 square feet
4. Scale of Effort: 35 percent
5. Production Data:
a. 1953 Production:
Airframe Weight Pounds per Year
Model (Pounds) Units per Year (including Spares)
MIG-15
or Variant
6,065 755 5,780,000
b. Capacity Production:
Year Model Units per Year
Pounds per Year
(including Spares)
1954 MIG-15
or Variant
1,282
9,800,000
1955 m10-15
or Variant
2,782
21,280,000
1956 MIG-15
or Variant
3)350
25,760,000
50X1
50X1
- 119 -
S-E-C -R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
6. Input Data:
Production
1953
1954
Capacity
1955
Capacity
1956
Capacity
a. Materials:
S-E-C-R-E-T
Yearly Gross Requirements
Metric Tons)
1
rd
0
H?-?
c.) H
0 a)
H a) co
-P
H 4-3 U) o
Ii) z ca
Hco o
Cr) 0)
H H al
(1)
3-1 CO -P
2
p..
0 M
a) H a) as
ro 4-> cc3
8 En 0 3-i U)
I.
0
OW a)
ri!--
4-1 1
P4
P4 0
g)
? rd
ea
a) a)
,a
,c1
0 H
Ea
co
a3
0 fa?
-JA-- 0
o
X 14 M C.5
126 2,180 20.4 1,940 147 8.6 17.8 35.4 - 51.1
and Plastics
213 3,690 34.7 3,280 211.9 14.7 30.2 6o.o 86.7
463 8,020 75.2 7,130 540 31.8 65.6 130 188
560 9,720 91.1 8,630 654 38.5 79.4 158 228
b.. Manpower:
Manpower.. Requirements
(Man-Years)
Mana- Tech-
Production Total Direct Indirect Skilled Unskilled gerial nical
1,760
5,040
5,040
5,040
1953
9,800
4,900
4,900
3,430
6,370
1,960
1954 Capacity
28,000
14,000
14,000
9,800
18,200
5,600
1955 Capacity
28,000
14,000
14,000
9,800
18,200
5,600
1956 Capacity
28,000
14,000
14,000
9,800
18,200
5,600
- 120
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C-R-E-T
? ? ? ? ? ?
c. Electrical Energy:
Source: Novosibirsk Heat and Power Plant
Alternate Source: Unknown
Electrical Energy Requirements
ProdUction (Kilowatt-Hours)
1953 14)500,000
1954 Capacity 41,300,000
1955 Capacity 41,300,000
1956 Capacity 11.1,300,000
d. Fuel and Lubricants:
Fuel Lubricants
Coal Lube Grease Lube Oil Cutting Oils
Production (Metric Tons) (Metric Tons) -(Gallons) (Gallons)
1953
43,700
2.29
17,100
6,340
1954 Capacity
78,400
6.54
48,900
18,100
1955 Capacity
78,400
6.54
48,900
18,100
1956 Capacity
78,400
6.54
48,900
18,100
- 121 -
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
e. Transportation:
S-E-C -R-E-T
Transportation Required
(Metric Tons)
Production
Products Transported to Plant
Products Transported
from Plant
Com- Raw
Engines ponents Materials
Fuel
Lubri- Spare
cants Aircraft Parts Scrap
1953
678
128
4,526.3
43,700
82.0
2,880
544
1,909
1954
Capacity
1,150
218
7,658.3
78,400
234.5
4,900
966
3,215
1955
Capacity
2,500
473
16,643.6
78,400
234.5
10,600
1,990
6,994
?
1956
Capacity
3,010
595
.20,159.0
78,400
234.5
12,800
2,11.80
8,479
- 122 -
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7 I
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
1. Plant Number:
S-E-C-R-E-T
2. Plant Location:
a. Nearest City and Coordinates: Omsk
b. Economic Region: IX
3. Plant Area: 1,075,000 square feet
4. Scale of Effort: 45 percent
5. Production Data:
a. 1953 Production:
Airframe Weight Pounds per Year
Model (Pounds) Units per Year (including Spares)
11-28 16,84o 276 5,160,000
b. Capacity Production:
Year
Model
Units per Year
Pouhds per Year
(including Spares)
1954
11-28
423
7,740,000
1955
11-28
714
13,060,000
1956
11-28
829
15,150,000
- 123
S-E-C-R-E-T
50X1
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
6. Input Data:
;-1
4-)
q-4
Production
1953
1954
Capacity
1955
Capacity
1956
Capacity
a. Materials:
S-E-C-R-E-T
Yearly Gross Requirements
(Metric Tons)
1
Ti
OH
0 a)
Cl)
-1-)
H 4-) 0 0
a) m
Ha) o
-1-) ?---- co
cr) a)
HH riD a)
0
9
a) it
GD
,0 -I-) cd
and Plastics
-i-)
(11 0 Cl)8 -)
.,, 0 a)
$...
a)
a) u)
o I ncl
gz) Cl)
cd
r-I 0
0 tt
9 P4
P4 P
.r4 0 o 0 H
0 4 1:4 0
N
P4 .1-1
98.3 1,690 15.9 2,950 103 9.1 4.7 145 16.4
147 2,530 23.9 4,420 154 13.7 7.0 218 24.6
249 4,270 40.2 7,460 260 23.1 11.8 367 41.4
288 4,960 46.7 8,650 302 26.8 13.7 426 48.1
b. Manpower:
Production
1953
1954 Capacity
1955 Capacity
1956 Capacity
Manpower Requirements
(Man-Years)
Mana- Tech-
Total Direct Indirect Skilled Unskilled gerial nical
6,450 3,225 3,255 2,260 4,190 1,290 1,160
14,340 7,170 7,170 5,020 9,320 2,870 2,580
14,340 7,170 7,170 5,020 9,320 2,870 2,580
14,340 7,170 7,170 5,020 9,320 2,870 2,580
- 124 -
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S -E -C-fl -E -T
c. Electrical Energy:
Source: Omsk Municipal Power Plant
Alternate Source: Unknown
Electrical Energy Requirements
Production (Kilowatt-Hours)
1953 9,620,000
1954 Capacity 21,200,000
1955 Capacity 21,200,000
1956 Capacity 21,200,000
d. Fuel and Lubricants:
Fuel Lubricants
Coal Lube Grease Lube Oil Cutting Oils
Production Metric Tons (Metric Tons) (Gallons) (Gallons)
1953
22,400
1.51
11,300
4,170
1954 Capacity
40,200
3.35
25,000
9,260
1955 Capacity
40,200
3.35
25,000
9,260
1956 Capacity
40,200
3.35
25,000
9,260
- 125 -
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
e. Transportation:
S-EC-R-E-T
Transportation Required
(Metric Tons)
Production
Products Transported to Plant
Products Transported
from Plant
Com- Raw
Engines ponents Materials
Fuel
Lubri- Spare
cants Aircraft Parts Scrap
1953
496
353
5,032.4
22,400
54.1
0
230
2,692
1954
Capacity
760
541
7,342.0
40,200
116.9
0
280
3,832
1955
Capacity
1,282
914
12,722.5
40,200
116.9
0
470
6,796
1956
Capacity
1,489
1,061
14,761.3
40,200
116.9
0
540
7,886
- 126 -
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C -R-E-T
1. Plant Number:
2. Plant Location:
a. Nearest City and Coordinates:
b. Economic Region: IV
3. Plant Area: 1,100,000 square feet
4. Scale of Effort: 30 Percent
5. Production Data:
a. 1953 Production:
Rostov
. Airframe Weight Pounds per Year
Model (Pounds) Units per Year (including Spares)
a
Yak-6
1,754
324
723,000
Yak-8
2,394
240
723,000
Yak-16
5,946
192
1,446,000
b. Capacity Production:
Pounds per .Year
Year Model (including Spares)
1954 AMFR weight under 20,000
pounds 5,780,000
1955 MEM weight under 20,000
pounds . 12,540,000
1956 ANTE weight under 20,000
pounds 15,180,000
- 127 -
S-E-C-R-E-T
50X1
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
6. Input Data:
Production
1953
1954
Capacity
1955
Capacity
1956
Capacity
a. Materials:
S-E-C-R-E-T
Yearly Gross Requirements
(Metric Tons)
I
rd
OH
0 a)
CO
4).
H -PCI) 0
Cl) 0 H H
a) u)
4-) .....,m
Cl) Cl)
HH 0
o a) ?H
Li 9
o a) 0
U)? 4)
gPLI ?,-1
d Cf) H O. P Ea P
0 Oa)
PI 0
0
rd
a3 do
,c)
a)
0
C.)
H 0
tIC)
P4
o Hr4 o
1
. o
__1=1..._. C.) I-4 z
51.1
891
8.3
1,140
72.1
94.4
1,600
15.2
2,780
105.0
205
3,480
33.0
6,030
228.0
248
4,210
39.9
7,300
275.0
b. Manpower:
Glass and Plastics
7.9 4.0 38.0 17.1
17.0 24.1 99.6 34.1
58.6 52.3 216 73.9
70.9 63.3 262 89.5
Manpower Requirements
(Man-Years)
Mana- Tech-
Production Total Direct Indirect Skilled Unskilled gerial nical
1953
4,400
2,200
2,.200
1,540
2,860
880
792
1954 Capacity
14,66o
7,330
7,330
5,130
9,530
2,930
2,640
1955 Capacity
14,660
7,330
7,330
5,130
9,530
2,930
2,640
1956 Capacity
14,66o
7,330
. 7,330
5,130
9,530
2,930
2,64c
- 128 -
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C-R-E-T
c. Electrical Energy:
Source: Rostov Municipal Power Supply
Alternate Source': Unknown
Electrical Energy Requirements
Production (Kilowatt-Hours)
1953
6,500,000
1954 Capacity
21,700,000
1955 Capacity
21,700,000
1956 Capacity
21,700,000
d. Fuel and Lubricants:
Production
Fuel
Lubricants
Coal
(Metric Tots)
Lube Grease
(Metric Tons)
Lube Oil
(Gallons)
Cutting 0i1S
(Gallons)
1953
12,800
1.03
7,680
2,840
1954 Capacity
23,000
3.42
25,600
9,480
1955 Capacity-
23,000
3.42
25,600
9,480
1956 Capacity
23,000
3.42
25,600
9,480
- 129 -
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
e. Transportation:
S-E-C -R-E-T
_ _ _ _ _
Transportation Required
(Metric Tons)
Production
Products Transported to Plant
Products Transported
from Plant
Com- Raw
Engines ponents Materials
Fuel
Lubri- Spare
cants Aircraft Parts Scrap
1953
299
223 2,229.5
12,800
36.8 0
243 946
1954
Un-
Capacity
Unknown Unknown 4,769.4
23,000
122.7 Unknown
known 2,206
1955
Un-
Capacity
Unknown
Unknown 10,376.8
23,000
122.7 Unknown
known 4,817
1956
Un-
Capacity
Unknown
Unknown 13,128.3
23,000
122.7 Unknown
known 6,393
- 130 - .
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
1. Plant Number:
S-E-C -R-E-T
2. Plant Location:
a. Nearest City and Coordinates:
b. Economic Region:
3. Plant Area: 305,000 square feet
4. Scale of Effort: 45 percent
5. Production Data:
a. 1953 Production:
Leningrad
50X1
Airframe Weight Pounds per Year
Model (Pounds) Units per Year (including Spares)
Yak-18 850
b. Capacity Production:
708 750,000
Pounds per Year
Year -Model (including Spares)
1954 AMPR weight under 20,000
pounds 2,060,000
1955 AMPR weight under 20,000
pounds 3,660,000
1956 AMPR weight under 20,000
pounds 4,300,000
- 131 -
S-E-C-R-E-T
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
6. Input Data:
Production
a. Materials:
S-E-C-R-E-T
Yearly Gross Requirements
(Metric Tons)
rd
OH
0
H --N
0 a)
CO
-I-)
H -P Er) 0
o o H H
o u)
co a)
H H a)
O a)?-1a)
)-1 ca -p
Cl)
2 0
fai gr-1
gli .H
9
ca
. a) a)
ro
003 : 00).a) a)
H 0
0 bi:) ?41 1:14
P4 0 rd ,c)
,c)
O e 0 g) a)
0
-13___ .4 .44 0 Z 1-1 14
Glass and Plastics
1953 11.6 197 1.8 361 14.0 0.0 1.6 3.0 4.4
1954
Capacity 33.6 572 5.4 990 37.4 9.6 8.6 35.5 12.1
1955
Capacity 59.8 1,020 9.5 .1,760 66.4 17.1 15.3 63.1 21.6
1956
Capacity 70.2 1,190 11.3 2,070 78.0 20.1 17.9 74.1 25.4
b. Manpower:
Manpower Requirements
(Man-Years)
Mana- Tech-
Production Total Direct Indirect Skilled Unskilled gerial nical
333
732
732
732
1953
1,850
925
925
650
1,200
370
1954 Capacity
4,070
2,035
2,035
1,420
2,650
814
1955 Capacity
4,070
2,035
2,035
1,420
2,650
814
1956 Capacity
4,070
2,035
2,035
1,420
2,650
814
- 132
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C-R-E-T
c. Electrical Energy:
Source: City Power Station
Alternate Source: Unknown
Production
Electrical Energy Requirements
(Kilowatt-Hours)
1953
21730,000
1954 Capacity
6,000,000
1955 Capacity
61000,000
1956 Capacity
6,000,000
d. Fuel and Lubricants:
Production
Fuel
Lubricants
Coal
(Metric Tons)
Lube Grease
Metric Tons)
Lube Oil
(Gallons)
Cutting Oils
(Gallons)
1953
4,730
0.43
3,200
1,180
1954 Capacity
8,480
0.95
7,110
2,630
1955 Capacity
81480
0.95
7,110
2,630
1956 Capacity
8,480
0.95
7,110
2,630
"
- 133 -
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
e. Transportation:
S-E-C-R-E-T
Transportation Required
(Metric Tons)
Production
Products Transported to Plant
Products Transported
from Plant
Com- Raw
Engines ponents Materials
Fuel
Lubri-
cants
Spare
Aircraft Parts Scrap
1953
138 122
594.4
4,730
15.3
512
67
254
1954
Un-
Capacity
Unknown Unknown
1,704.2
8,480
34.0
Unknown
known
770
1955
Un-
Capacity
Unknown Unknown
3,032.8
8,IA0
34.0
Unknown
known
1,373
1956
?
Un-
Capacity
Unknown Unknown
3,557.0
8,480
34.0
Unknown
known
1,606
- 134 -
S -E -C -R -E -T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C-R-E-T
1.
2.
Plant Number:
Saratov
50X1
Plant Location:
a. Nearest City and Coordinates:
b. Economic Region: VI
50X1
3.
Plant Area: 1,400,000
square feet
4.
Scale of Effort:
45 percent
5.
Production Data:
a. 1953 Production:
Airframe Weight pounds per Year
Model (Pounds) Units per Year (including Spares)
MIG-15
or Variant
6,065 1,020 6,132,000
b. Capacity Production:
Year Model
Units per Year
Pounds per Year
(including Spares)
1954 MIG-15
or Variant
1,390
8,400,000
1955 MIG-15
or Variant
2,475
14,950,000
1956 MIG-15
or Variant
2,910
17,550,000
-135-
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
6. Input Data:
a. Materials:
S-E-C-R-E-T
Yearly Gross Requirements
Metric Tons)
I
r0
OH
.,--1 1a)
;-, ,-4 a) co
o 4-)
-I-) H -1-) VI o
d a) 0 H H
W ta W
.p ,-., d W
cl--1) Cf) 4-)
o 1 r cn
Ni? a)
. ..-I
M
0
9
,0 .0 0
M
at
1 1
o ? m 4-)
m g' ;-. TA
0
0 . . . o
H ..0 .1-1
0 "d g4
P4g rd
0 r0
rC, 0
d
Obi)
Production -Ja...... H
O -1-1 o o H
1953
1954
Capacity
1955
Capacity
1956
Capacity
b.
Production
133 2,310
21.7
2,060 156 9.2
18.9
37.5
54.2
183 3,170
29.7
2,820 213 12.6
25.9
51.4
74.3
325 5,640
52.9
5,010 380 22.4
46.1
91.6
132
382 6,620
62.1
5,880 446 26.3
54.2
108
155
Manpower:
Manpower Requirements
(Man-Years)
Mana-
Tech-
Total
Direct
Indirect Skilled Unskilled
gerial
nical
1953
8,490
4,245
4,245
2,970
5,520
1,700
1,530
1954 Capacity
18,660
9,330
9,330
6,530
12,130
3,730
3,360
1955 Capacity
18,660
9,330
9,330
6,530
12,130
3,730
3,360
1956 Capacity
18,660
9,330
9,330
6,530
12,130
3,730
3,360
- 136.-
S -E -C -R-E-T
_ _ _ _ _ _
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C-R-E-T
c. Electrical Energy:
Source: Saratov TETS II
Alternate Source: Plant power station
Production
Electrical Energy Requirements
(Kilowatt-Hours)
1953
121500,000
1954 Capacit3
27,600,000
1955 Capacity
27,600,000
1956 Capacity
27,600,000
d. Fuel and Lubricants:
Fuel Lubricants
Production
Coal
(Metric Tons)
Lube Grease
(Metric Tons)
Lube Oil
(Gallons)
Cutting Oils
(Gallons)
1953
20,800
1.96
14,700
5,440
1954 Capacity
37,200
4.37
32,600
12,100
1955 Capacity
37,200
4.37
32,600
12,100
1956 Capacity
37,200
4.37
32,600
12,100
-137-
S-E-C -R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
e. Transportation:
S-E-C-R-E-T
Transportation Required
(Metric Tons)
Production
Products Transported to Plant
Products Transported
from Plant
Com- Raw
Engines ponents Materials
Fuel
Lubri- Spare
cants Aircraft Parts Scrap
1953
916
173
4,800.5
20,800
70.5 3,900 0 2,120
1954
Capacity
1,250
236
6,579.9
37,200
156.4
5,310
0
2,770
1955
Capacity
2,220
421
11,700.0
37,200
156.4
9,460
0
4,920
1956
Capacity
2,610
495
13,733.6
37,200
156.4
11,100
0
5,774
-138-
S-E -C -R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
1. Plant Number:
S-E-C-R-E-T
2. Plant Location:
a. Nearest City and Coordinates: Moscow
b. Economic Region: VII
3. Plant Area: 605,000 square feet
4. Scale of Effort: 45 percent
5. Production Data:
a. 1953 Production:
Airframe Weight Pounds per Year
Model (Pounds)
Un-
known
Unknown
b. Capacity Production:
Units per Year (including Spares)
Unknown Unknown
Pounds per Year
Year -Model (including Spares)
1954 AMP?' weight under 20,000
pounds 4,080,000
1955 AMPR weight under 20,000
pounds 7,260,000
1956 AMPR weight under 20,000
8,520,000
-139-
S-E-C -R-E-T
50X1
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
6. Input Data:
Production
1953
1954
Capacity
1955
Capacity
1956
Capacity
a. Materials:
Type of Material
S-E-C-R-E-T
Yearly Gross Requirements
(Metric Tons)
IlL ow-Carbon Steel
66.6
1,130
119
2,020
139
2,370
b. Manpower:
Stainless Steel
co Cr)
0
o ..-1
H +3
Cl)
d
H
W P-1
3.4 u)
a) a3 rd
fo4 Pc1
M 0
A (Ti
O ;-4 (0
00.) o o Cl)
p40
rg go Cl)
P4
W 4:) (Ti
O a) H'
0 Z
10.7 1,960 74.0 19.1 17.0 70.3 24.1
19.1 3,490 132 33.9 30.3 125 42.8
22.4 4,100 155 39.9 35.6 147 50.3
Manpower Requirements
(Man-Years)
Mana- Tech-
Production Total Direct Indirect Skilled Unskilled gerial nical
1953
1954 Capacity
1955 Capacity
1956 Capacity
3,670
1,835
1,835
1,290
2,380
734
660
8,070
4,035
4,035
2,830
5,240
1,240
1,450
8,070
4,035
4,035
2,830
5,240
1,240
1,450
8,070
4,035
4,035
2,830
51240
11240
1,450
S-E-C -R-E-T
_ _ _ _
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01.141A000300080002-7
S-E-C-R-E-T
c. Electrical Energy:
Source: Outside, probably supplied by Moscow city system
Alternate Source: Unknown
Electrical Energy Requirements
Production (Kilowatt-Hours)
1953
5142o,000
1954 Capacity
11,900,000
1955 Capacity
11,900,000
1956 Capacity
11,900,000
d. Fuel and Lubricants:
Production
Fuel
Lubricants
Coal
(Metric Tons)
Lube Grease
(Metric Tons)
Lube Oil
(Gallons)
Cutting Oils
(Gallons)
1953
9,440
0.85
6,340
2,350
1954 Capacity
16,900
1.89
14,100
5,220
1955 Capacity
16,900
1.89
14,100
5,220
1956 Capacity
16,900
1.89
14,100
5,220
- 141 -
S-E -C -R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
e. Transportation:
S-E-C-R-E-T
Transportation Required
(Metric Tons)
Production
Products Transported to Plant
Products Transported
from Plant
Com- Raw
Engines ponents Materials
Fuel
Lubri- Spare
cants Aircraft Parts Scrap
1953
Unknown Unknown
Unknown
9,440
30.4 Unknown
Un- , Un-
known known
1954
Un-
Capacity
Unknown Unknown
3,371.8
16,900
67.6 Unknown
known 1,522
1955
Un-
Capacity
Unknown Unknown
6,012.1
16,900
67.6 'Unknown
known 2,720
1956
Un-
Capacity
Unknown Unknown
7,059.2
16,900
67.6 Unknown
known 3,190
- 142 -
S -E -C -R -E -T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
1. Plant Number:
S-E-C-R-E-T
2. Plant Location:
a. Nearest City and Coordinates: Moscow
b. Economic Region: VII
Plant Area: 668,000 square feet
I. Scale of Effort: 1-5 percent
5. Production Data:
a. 1953 Production:
Airframe, Weight Pounds per Year
Model (Pounds) Units per Year (including Spares)
Subcontracting
b. Capacity Production:
Pounds per Year
Year Model (including Spares)
1954 AMPR weight under 20,000
pounds 4,512,000
1955 AMPR weight under 20,000
pounds 8,016,000
1956 AMPR weight under 20,000
pounds 9,420,000
- 143 -
S-E-C-R-E-T
50X1
50X11
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
6. Input Data:
Production
1953
a. Materials:
S-E-C-R-E-T
Yearly Gross Requirements
(Metric Tons)
Stainless Steel
Cl)
0
H
a)
P TI
(fili 14
PI
Pi
0 i?-( W
(D (U
Cal 0 qd ro
Pi
W (TS r0
o a)
? 0 Z e-4 C4
and Plastics
1954
Capacity 73.7 1,250 11.9 2,170 81.8 21.1 18.8 77.8 26.6
1955
Capacity 131.0 2,230 21.1 3,850 145.0 37.5 33.4 138.0 47.3
1956
Capacity 154.0 2,620 24.8 4,530 171.0 44.0 39.3 162.0 55.6
b. Manpower:
Manpower Requirements
(Man-Years)
Mana- Tech-
Production Total Direct Indirect Skilled Unskilled gerial nical
1953
1954 Capacity
1955 Capacity
1956 Capacity
4,050
2,025
2,025
1,420
2,630
810
729
8,910
4,455
4,455
3,120
5,790
1,780
1,600
8,910
4,455
' 4,455
3,120
5,790
1,780
1,600
8,910
4,455
4,455
3,120
5,790
1,780
1,600
- 144 -
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7 I
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C-R-E-T
c. Electrical Energy:
Source: Moskva City Supply
Alternate Source: Plant emergency station
Production
Electrical Energy Requirements
(Kilowatt-Hours)
1953
5,980,000
1954 Capacity
13,100,000'
1955 Capacity
13,100,000
1956 Capacity
13,100,000
d. Fuel and Lubricants.
Production
Fuel
Lubricants
Coal
(Metric Tons)
Lube Grease
(Metric Tons)
Lube Oil
(Gallons)
Cutting Oils
(Gallons)
1953
10,300
0.94
7,020
2,590
1954 Capacity
18,700
2.09
15;600
5,760
1955 Capacity
18,700
2.09
15,600
5,760
1956 Capacity
18,700
2.09
15,600
5,760
-145-
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
e. ?Transportation:
S-E-C-R-E-T
Transportation Required
(Metric Tons)
Production
Products Transported to Plant
Products Transported
from Plant
Com- Raw
Engines ponents Materials
Fuel
Lubri- Spare
cants Aircraft Parts Scrap
1953
Unknown Unknown
Unknown
10,300
33.6
Unknown
Un- Un-
known known
1954
Un-
Capacity
Unknown Unknown
3,731.7
18,700
74.7
Unknown
known 1,684
1955
Un-
Capacity
Unknown Unknown
6,633.3
18,700
74.7
Unknown
known 2,998
1956
Un-
Capacity
Unknown Unknown
7,800.7
18,700
74.7
Unknown
known 3,528
-146-
S -E -C -R -E -T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C-R-E-T
1. Plant Number:
2. Plant Location:
a. Nearest City and Coordinates:
b. Economic Region: I
3. Plant Area: 401,000 square feet
Is.. Scale of Effort: 45 percent
5. Production Data:
a. 1953 Production:
Leningrad
50X1
50X1
Airframe Weight Pounds per Year
Model (Pounds) Units per Year (including Spares)
Yak-11 2,500 312 987,000
b. Capacity Production:
Pounds per Year
Year Model (including Spares)
1954 AMPR weight under 20,000
pounds 2,700,000
1955 AMPR weight under 20,000
pounds , 4,810,000
1956 AMPR weight under 20,000
pounds 5,650,000
- 147 -
S-E-C -R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
6. Input Data:
Production
1953
1954
Capacity
1955
Capacity
1956
Capacity
a. Materials:
0
-P
0
0
ti)
S-E-C-R-E-T
Yearly Gross Requirements
(Metric Tons)
rd
0
4-1 ^
OH
O 0
-r1 CD Cl) Cl)
-P 0
H -I-DUD 0 ..-1
0
O M
0
H
-1-)
Cl)
-1-) s?-?-' (1) d
M a) H
HH 0 114
O 0 0 P d
O a) ?H 0 d nzi
d
P
(/) 4.)
ED g 0 P
g14 PE1
9
U)
d
C) ..4 ,-) ri W 0 0 co
H 003
OO d M
0 Pi
PI 0 r
W r0
r0
d
_la__ _.:L_ 0
Z
)
I-1
r4
0
C!)
O L o g m H
11.2
190
44.1
750
78.5
1,330
?92.2
1,570
b. Manpower:
1.8 64o 13.4 8.1 0.0 11.2 7.2
7.1 1,300 49.0 12.6 11.3 46.5 15.9
12.6 2,310 87.2 22.5 20.1 82.8 28.3
14.9 2,720 103 26.4 23.6 97.4 33.3
Manpower Requirements
(Man-Years)
Mana- Tech-
Production Total Direct Indirect Skilled Unskilled gerial nical
1953
1954 Capacity
1955 Capacity
1956 Capacity
2,430
1,215
1,215
850
1,580
486
437
5,350
2,675
2,675
1,870
3,480
1,070
963
5,350
2,675
2,675
1,870
3,480
1,070
963
5,350
2,675
2,675
1,870
3,480
1,070
963
- 148 -
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
c. Electrical Energy:
Source: Probably GRES
Alternate Source: Unknown ,
S-E-C-R-E-T
Leningrad
Production
Electrical Energy Requirements
(Kilowatt-Hours)
1953
3,5900000
1954 Capacity
7,900,000
1955 Capacity
7,900,000
1956 Capacity
7,900,000
d. Fuel and Lubricants:
Production
Fuel
Lubricants
Coal
(Metric Tons)
Lube Grease
(Metric Tons)
Lube Oil
(Gallons)
Cutting Oils
(Gallons)
1953
6,220
0.56
4,200
1,560
1954 Capacity
11,100
1.25
9,340
3,460
1955 Capacity
11,100
1.25
9,340
3,460
1956 Capacity
11,100
1.25
9,340
3,460
- 149 -
S-E-C-R-E-T
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
e. Transportation:
S-E-C-R-E-T
Transportation Required
(Metric Tons)
Production
Products Transported to Plant
Products Transported
from Plant
Com- Raw
Engines ponents Materials
Fuel
Lubri- Spare
cants Aircraft Parts Scrap
.1953
152 76
882.9
6,220
20.2 627
94 435
1954
Un-
Capacity
Unknown Unknown
2,236.5
11,100
44.8 Unknown
known 1,011
1955
Un-
Capacity
Unknown Unknown
3,972.0
11,100
44.8 Unknown
known 1,790
1956
Un-
Capacity
Unknown Unknown
41680.8
11,100
44.8 Unknown
known 2,120
- 150 -
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
1. Plant Number:
S-E-C-R-E-T
2. Plant Location:
a. Nearest City and Coordinates: Moscow
b. Economic Region: VII
3. Plant Area: 330,000 square feet
4. Scale of Effort: 45 percent
5. Production Data:
a. 1953 Production:
50X1
Airframe Weight Pounds per Year
Model (Pounds) Units per Year (including Spares)
Yak-12 807 240 240,000
Type 24 6,300 168 1,386,000
b. Capacity Production:
Pounds per Year
Year Model (including Spares)
1954 AMPR weight under 20,000
pounds 2,230,000
1955 AMPR Weight under 20,000
pounds 3,960,000
1956 AMFR weight under 20,000.
.pounds 4,650,000
- 151 -
A S-E-C -R-E -T
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
6. Input Data:
Production
1953
1954
Capacity
1955
Capacity
1956
Capacity
0
cd
a. Materials:
S-E-C-R-E-T
Yearly Gross Requirements
(Metric Tons)
1
rd
H ---N
c) H
0 a)
Cl)
4-)
H 4-) cr) o
w o H H
a) M Cl) a)
_p ?'U), a)
rn-1-3
O Zi r) CO
$4 u)
a)
9
Pi P:1
.1-1
9
O (1) 4-1 Cl)
a) d
P
$4
4
(1)4-)
0 r)
-? a)
d m o s-1
0
o g 1,1 M pi
0
1jH tilo
_JA__ o
20.7 353 3.3 846 22.2
36.4 619 5.9 1,070 40.5
64.7 1,100 10.4 1,900 71.9
76.0 1,290 12.2 21240 84.4
b. Manpower:
u)
o
W
X
w
o
14
w
ro
.0
o
C4
0.0
2.6
5.0
11.4
9.3
38.4
18.5
16.5
68.3
21.7
19.4
80.2
Manpower Requirements
(Man-Years)
Glass and Plastics
7.6
13.2
23.4
27.4
Mana- Tech-
Production . Total Direct Indirect Skilled Unskilled gerial nical
1953
1954 Capacity
1955 Capacity
1956 Capacity
2,000
1,000
1,000
700
1,300
400
360
4,400
2,200
2,200
1,540
2,860
880
792
4,400
2,200
2,200
1,540
2,860
880
792
4,400
2,200
2,200
1,540
2,860
880
792
- 152 -
S-E-C-R-E-T
? ? ? ? ? ?
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C-R-E-T
c. Electrical Energy:
Source: Moscow City Grid
Alternate Source: Plant power Station
Production
Electrical Energy Requirements
(Kilowatt-Hours)
1953
2,950,000
1954 Capacity
6,500,000
1955 Capacity
6,500,000
1956 Capacity
6,500,000
d. Fuel and Lubricants:
Production
Fuel
Lubricants
Coal
(Metric Tons)
Lube-Grease
(Metric Tons)
Lube Oil
(Gallons)
Cutting Oils
(Gallons)
1953
5,150
0.46
3,460
1,280
1954 Capacity
9,240
1.03
7,690
2,840
1955 Capacity
9,240
1.03
7,690
2,840
1956 Capacity
9,240
1.03
7,690
2,840
- 153 -
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
e. Transportation:
S-E-C-R-E-T
Transportation Required
(Metric Tons)
Production
Products Transported to Plant
Products Transported
from Plant
Com- Raw
Engines ponents Materials
Fuel
Lubri- Spare
cants Aircraft Parts Scrap
1953
47 39
1,260.4
5,150
16.5
480
170 522
1954
Un-
Capacity
Unknown Unknown
1,844.1
9,240
36.8
Unknown
known 833
1955
Un-
Capacity
Unknown Unknown
3,273.7
9,240
36.8
Unknown
known 1,478
1956
Un-
Capacity
Unknown Unknown
3,851.3
9,240
36.8
Unknown
known 1,741
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S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
1. Plant Number:
S-E-C-R-E-T
2. Plant Location:
a. Nearest City and Coordinates:
b. Economic Region: III
3. Plant Area: 268,334 square feet
4. Scale of Effort: 45 percent
5. Production Data:
a. 1953 Production:
Kiev
Airframe Weight Pounds per Year
Model (Pounds) Units per Year (including Spares)
AN-2
3,500
132
558,000
Type 36
4,710
55
321+,000
b. Capacity Production:
Year Model Units per Year
Pounds per Year
(including Spares)
1954
Type 36
377 ?
1,810,000
1955
Type 36
671
3,220,000
1956
Type 36
788
3,780,000
-155-
S-E-C-R-E-T
50X1
50X1
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Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
6. Input Data:
a. Materials:
Type of Material
Production
S-E-C-R-E-T
Yearly Gross Requirements
(Metric Tons)
IL ow-Carbon Steel
Stainless Steel
ta
0
H
a)
P m
a) a3
9
RI Irl
R4 .1-1
O P w
ow a) a)
RI 0 'CI r0
P4
W as ro
o
o Z 1-4 P4
Glass and Plastics
1953 23.4 408 3.8 410 20.1 46.6 1.2 4.o 6.8
1954
Capacity 83.0 1,430 13.1 862 59.9 26.0 0 9.9 19.7
1955
Capacity 148 2,254 23.4 1,530 107 46.3 0 17.5 35.0
1956
Capacity 176 2,990 27.4 1,800 125 54.4 0 20.6 41.2
b. Manpower:
Manpower Requirements
(Man-Years)
Mana- Tech-
Production Total Direct Indirect Skilled Unskilled gerial nical
1953
1,630
815
570
1954 Capacity
3,580
1,790
1,790
1955 Capacity
3,580
1,790
1,790
,
1956 Capacity
3,580
1,790
1,790
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S-E-C,R-E-T
570
1,060
326
293
1,250
2,330
716
644
1,250
2,330
716
644
1,250
2,330
716
611.11.
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
S-E-C-R-E-T
c. Electrical Energy:
Source: City Plant
Alternate Source:
Production
Plant emergency generator
Electrical Energy Requirements
(Kilowatt-Hours)
?
1953
2,400,00o
1954 Capacity
5,280,000
1955 Capacity
5,280,000
1956 Capacity
5,280,000
d. Fuel and Lubricants:
Production
Fuel
Lubricants
Coal
(Metric Tons)
Lube Grease
(Metric Tons)
Lube Oil
(Gallons)
Cutting Oils
(Gallons)
1953
3,320
0.38
2,820
1,040
1954 Capacity
5,956
0.84
6,260
2,310
1955 Capacity
5,950
. 0.84
6,260
2,310
1956 Capacity
5,950
0.84
6,260
2,310
- 157 -
S-E-C-R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
e. Transportation:
S-E-C-R-E-T
_ _ _ _ _
Transportation Required
(Metric Tons)
Production
Products Transported to Plant
Prdducts Transported
from Plant
Com- Raw
Engines ponents Materials
Fuel
Lubri- Spare
cants Aircraft Parts Scrap
1953
114
51
923.9
3,320
13.5
0
73
597
1954
Capacity
203
81
2,503.6
5,950
29.9
0
164
1,683
1955
Capacity
360
144
4,447.2
5,950
29.9
0
302
2,976
1956
Capacity
423
169
5,231,6
5,950
29.9
0
341
3,518
- 158 -
S-E-C -R-E-T
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
50X1
Declassified in Part - Sanitized Copy Approved for Release 2013/12/12 : CIA-RDP79R01141A000300080002-7
R
11,050X1
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# glif 50X1
4Z006?1
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