MILITARY THOUGHT (USSR): COMBAT EMPLOYMENT OF ORBITAL AIRCRAFT

• Document Type: CREST
• Collection: General CIA Records
• Document Number (FOIA) /ESDN (CREST): CIA-RDP10-00105R000100130001-1
• Release Decision: RIPPUB
• Original Classification: T
• Document Page Count: 16
• Document Creation Date: December 22, 2016
• Document Release Date: September 26, 2012
• Sequence Number: 1
• Publication Date: June 4, 1973
• Content Type: MEMO

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WASHINGTON, D.C. 20505
4 June 1973
MEMORANDUM FOR: The Director of Central Intelligence
SUBJECT MILITARY THOUGHT (USSR): Combat Employment
of Orbital Aircraft
1. The Enclosed Intelligence Information Special Report
is part of a series now in preparation based on the SECRET
USSR Ministry of Defense publication Collection of Articles
of the Journal "Military Thought." This article discusses the
principles of employment of strategic aerospace weapons
systems. Operational concepts are described both for orbital
systems and those operating in low and near space zones.
Missions for such systems are identified as weapon delivery,
reconnaissance, and destroy or capture action against hostile
spacecraft. This article appeared in Issue No. 2 (75) for
1965.
2. Because the source of this report is extremely sensi-
tive, this document should be handled on a strict need-to-know
basis within recipient agencies.
Depu y Director or era ions
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FIRDB-312/02676-73
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Distribution:
The Director of Central Intelligence
The Director of Intelligence and Research
Department of State
The Joint Chiefs of Staff
The Director, Defense Intelligence Agency
The Assistant to the Chief of Staff for Intelligence
Department of the Army
The Assistant Chief of Naval Operations (Intelligence)
Department of the Navy
The Assistant Chief of Staff, Intelligence
U.S. Air Force
Office of the Assistant to the President for
National Security Affairs
Deputy Director of Central Intelligence
Deputy Director for Intelligence
Deputy Director for Science and Technology
Director of Strategic Research
Director of Scientific Intelligence
Foreign Missile and Space Analysis Center
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COUNTRY USSR
DATE OF Mid-1965
INFO.
Intelligence Information Special Reper,1-HUM
SUBJECT
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DATE
4 June 1973
MILITARY THOUGHT (USSR): Problems of the Combat Use
of Orbital Aircraft
SOURCE Documentary
SUMMARY
The following report is a translation from Russian of an
article which appeared in Issue No. 2 (75) for 1965 of the
SECRET USSR Ministry of Defense publication Collection of
Articles of the Journal "Military Thought." The author of this
article is Colonel V. Odintsov. He asserts that aerospace
combat vehicles represent a new phase in the development of
strategic weapons and reconnaissance systems. He defines these
as manned and unmanned earth satellites and aerospace aircraft
capable of operating both within the upper limits of the
atmosphere and across into low space areas. Advantages over
existing strategic attack systems, as well as limiting factors
on aerospace systems such as maneuverability, are described in
principle in the article. Destruction or capture of hostile
space vehicles are identified as primary missions for aerospace
weapons systems.
COMMENT:
END OF SUMMARY
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Colonel V. A. Odintsov coauthored a reference book on
cosmonautics with General-Mayor N. Ya. Kondratyev which was
reviewed in the Air Defense Herald, Issue No. 11 for 1966.
Military Thought has been published by the USSR Ministry of
Defense in three versions in the past--TOP SECRET, SECRET,
and RESTRICTED. There is no information as to whether or not
the TOP SECRET version continues to be published. The SECRET
version is published three times annually and is distributed
down to the level of division comm5oxi-Hum
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Problems of the Combat Use of Orbital Aircraft
by Colonel V. Odintsov
The effectiveness of the employment of nuclear armament, and
therefore the course of armed combat, depends in a decisive way
on the availability of delivery vehicles capable of delivering
nuclear weapons to their targets. As is known, such strategic
delivery vehicles presently include intercontinental and inter-
mediate-range missiles, missile submarines, and missile-carrying
aircraft with a wide radius of operation.
Each type of delivery vehicle has its own inherent combat
characteristics. Thus, with strategic long-range missiles it is
possible to strike targets at great distances in a short time.
Aircraft have the advantages of practically unlimited maneuver-
ability in the air and the capability of independently finding
and destroying various land and sea targets (including moving
targets). Missile submarines can remain for extended periods on
lines of communication in the most remote areas of ocean theaters
of military operations.
However, there is no one perfect delivery vehicle at the
present time, and the capabilities of all existing delivery
vehicles are contained within well-defined and often very rigid
limits. For example, regardless of whether they are launched
from stationary installations or from submarines, missiles can
be used only against targets whose coordinates are determined in
advance; after the missiles are launched, it is difficult or
impossible to retarget them. Aircraft are not always able to
assure the necessary operational range and swiftness of strike
and also overcome strong air defenses.
Therefore, the perfection of existing strategic delivery
vehicles and the development of the most effective and economical
new delivery vehicles represent the most vital problems in the
development of our Armed Forces.
At the present time a new direction has been defined in the
development of delivery vehicles for nuclear weapons and recon-
naissance systems--the development of aerospace combat vehicles
capable of striking various targets and of conducting strategic
and operational reconnaissance. Depending on the region of
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space in which these vehicles are to be used, they can be condi-
tionally divided into two gills. The first consists of earth
satellites and spaceship-satellites for extended flight at
relatively high altitudes, from 200 to 250 kilometers and hicther.
The two types of satellites are distinguished from each other
principally by whether they are or are not manned; earth satel-
lites are unmanned space vehicles, while spaceship-satellites may
carry a crew. The maneuverability of this type of space vehicle
is very limited, while the majority of earth satellites cannot
maneuver at all.
The second group consists of !Face aircraft--orbital ar191
aerospace--capable of flying at low space altitudes (60 to 150
),silimatess). where the density of the atmosphere is fairly high
in comparison with other parts of space.
Orbital and aerospace aircraft presuppose the presence of
a crew, are launched from delivery aircraft, and land like
ordinary aircraft. Orbital aircraft can complete only two to
five orbits at low altitudes, while aerospace aircraft can main-
tain flight for many days.
From the viewpoint of technical realization, orbital aircraft
may be regarded as an immediate prospect in the development of
space aircraft. As regards aerospace aircraft, their development
requires the solution of numerous technical problems, and this
type of flying vehicle will therefore be the next stage in the
development of space weapons systems. However, the general
principles governing the combat application of aerospace aircraft
will in many respects be analogous to those of orbital aircraft.
On the whole the problem of the development and use of space
aircraft is already expanding beyond the limits of purely theo-
retical research and is assuming features of reality. However,
it is a very broad and complex problem. For this reason, the
present article will review some of the positions on the role of
orbital aircraft in armed combat and the principles governing the
combat use of these aircraft.
Let us dwell, first of all, on those circumstances which
have made it expedient to develop and produce orbital aircraft.
The development of space weapons systems is subject to the
same rules as the development of other types of armament. Means
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of attack and defense are being created simultaneously for combat
in space. Therefore, one of the indispensable requirements of
space weapons systems is to be able to fulfil their objectives
successfully even if the enemy has antispace defenses. An
analysis of the capabilities of space vehicles to overcome anti-
space defenses shows that their capabilities will be greatest at
a flight altitude of 60 to 120 kilometers. This is explained by
the fact that the distance at which space targets can be detected
at these altitudes by radar and optical equipment on the ground
is not great enough to enable antispace defense measures to be
taken in time to intercept and destroy the space targets. It is
in this range that orbital aircraft are to operate, which gives
them substantial advantages over vehicles flying at higher alti-
tudes. We may draw an analogy here with aerodynamic means whose
capabilities for overcoming antiaircraft defenses reach their
maximum at the low altitudes of 50 to 300 meters.
Another important feature of orbital aircraft is that they
are more capable of maneuvering in flight than are other types
of space vehicles.
It is known that at an altitude of 150 kilometers the
density of the atmosphere is so low (tens of thousands of times
less than on the ground) that it is practically impossible to
use aerodynamic lift for maneuvering to gain altitude or change
direction. Therefore the maneuvering of space vehicles at these
and higher altitudes can only be accomplished with the help of
special rocket engines. This is called rocket maneuvering, as
distinct from aerodynamic maneuvering in which aerodynamic
forces are exploited. If rocket and aerodynamic forces are used
together, the term combined maneuvering is applied.
With the present nature of fuel used in the maneuvering
engines of space vehicles, capabilities for changing direction
by rocket maneuvering are estimated at only four to six degrees.
To change the orbital plane by 15 to 20 degrees, however, requires
almost as much fuel as to launch a space vehicle. As a result,
rocket maneuvering, the only possible type for earth satellites
and spaceship-satellites, can be used only for small deviations
from the original orbit (for correctional, defensive, and landing
maneuvers).
One of the ways to increase the maneuver capability of
spaceship-satellites is to use composite space systems, in which
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a fuel compartment is launched separately into space and is joined
to the basic ship. Under combat conditions, however, the problem
of mating will be a complex and vulnerable part of the system.
Maneuver capabilities increase significantly with the com-
bined use of rocket and aerodynamic forces, but this is possible
only for space aircraft capable of flying at near space altitudes.
Combined maneuvering at altitudes on the order of 100 kilometers
makes it possible to double the maneuver capabilities of a space
vehicle. Descent into the denser atmospheric layers from 30 to
60 kilometers above the surface creates even more favorable con-
ditions for maneuvering, to a maximum of several tens of degrees.
A vehicle in flight may maneuver in order to increase the proba-
bility of avoiding antispace defenses, to widen the choice of
targets and the axes of approach to them, and to make another
approach to a particular target from a second orbit.
The positive qualities of orbital aircraft also include
relatively great economy of operation. It must be taken into
account that in order to fulfil combat tasks successfully with
a minimum expenditure of forces and means, it is necessary not
only to detect the target and determine its coordinates but also
to acquire a target image of sufficiently large size. In par-
ticular, this will make it possible in actions against large
target areas to destroy individual critical elements of the tar-
get without destroying the entire target area. The demands on
strike means in such actions may be appreciably reduced, depending
on the nature of the target and the location of its critical
elements. Detailed reconnaissance becomes extremely important here.
Thus, in actions against carrier strike large units, for ex-
ample, it is necessary to know the combat formation of the ships
and to determine the location of the strike carriers and ships
acting as false targets. At the same time, in order to be able
to fulfil tasks for destroying individual pinpoint targets and
critical small elements of area targets, we must increase the
_trike acruracy ofr attack mean. Unguided weapons of destruc-
tion dropped from space vehicles have a probable deviation of
several kilometers. Such a low level of accuracy will require
strike weapons of unjustifiably great power in order to destroy
the most critical strategic targets.
The use of orbital aircraft with sufficiently reliable
navigation and guidance systems makes it possible to acquire
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large-scale target images while carrying out reconnaissance
missions and to significantly increase the accuracy of strike
weapons; this will create conditions for more economical and
effective use of nuclear strike weapons. At the same time, the
guidance system, which assures radar contact with the target,
makes it possible to pick out errors in our determination of
target coordinates and in the delivery vehicle's course toward
the launch point of its weapons.
Finally, and also of great Importance, orbital aircraft
serving as delivery vehicles are capable of autonomous action.
This quality, a characteristic of aircraft, enables the crews of
space aircraft to carry out independent search and destruction
actions against critical enemy targets in a given area and also
to perform retargeting over a fairly broad zone.
The crew of a reconnaissance orbital aircraft, for example,
will be able to evaluate the situation, complete an initial re-
view of reconnaissance data, transmit the most urgent and vital
information to their command point or to other orbital aircraft,
make expedient decisions on the basis of available information,
systematically exploit their reconnaissance resources, provide
target designation for strategic missiles and nuclear submarines
and carry out other missions not achievable with unmanned flying
vehicles.
In carrying out tasks for the destruction of targets, a
crew may conduct active target search, perform the guidance of
strike weapons of the "space-to-earth" type, monitor the results
of a strike by orbital aircraft and other strategic weapons,
carry out retargeting tasks, and take measures to inhibit the
effectiveness of enemy countermeasures.
Let us look briefly at the main combat characteristics
determining the capabilities of orbital aircraft for use in
combat. In principle, orbital aircraft launched from a cosmo-
drome in the Soviet Union can proceed to any point above the
earth after completing one orbit. Starting from a given launch
point, a space aircraft may approach its target from two axes,
one of which, the main (shortest) one, assures reaching the
target in the minimum time, while the other approach, the
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The choice of the approach axis to a given target depends
above all on exactly how the situation develops, on the organi-
zation of enemy antispace defenses, and on the general plan of
use of strategic forces in mounting nuclear strikes. Thus, if
orbital aircraft are obliged to proceed against assigned targets
before our ballistic missiles have crossed the detection line,
then, regardless of the type and disposition of antispace defense
weapons, the main approach axes will be used in most instances in
order to shorten the total strike time. On the other hand, if
circumstances are such that space aircraft can take off appre-
ciably before the ballistic missiles are launched, and if this
does not reveal the overall plan of a massive strike, then the
approach may be along the auxiliary axes, especially if this
facilitates overcoming enemy antispace defense systems.
In choosing the approach of a space aircraft to its target,
consideration must be given to such factors as the axis on which
the space aircraft is launched, natural light conditions, assur-
ance of communications with command points, coordination of
actions with those of other types of strategic delivery vehicles
and with reconnaissance, time available for reaching assigned
targets, etc.
Launch axes of space aircraft can be divided into eastern,
western, and polar. Launch toward the east is most economical
from the viewpoint of energy expenditure, since the space vehicle
acquires initial velocity based on the rotation of the earth.
However, in a combat situation, the decisive factor in choosing
the launch axis may not be the energy expenditure factor but
other factors, such as the general plan for the use of delivery
vehicles, the time available, or other factors assuring high
effectiveness in the fulfilment of the combat mission.
It must be noted that the establishment of an approach on
two fixed axes to a given target prevents maximum exploitation of
the element of surprise and facilitates enemy organization of
antispace defenses.
What are the possibilities for widening the sector
of orbital aircraft to assigned targets? First of all,
the geographical position of our territory, we can move
launch points. Thus, with launch points located in the
between 50 and 60 degrees latitude, a ten-degree change
of approach
considering
the surface
area
in the
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longitude of the launch point will make possible a change of five
to six degrees in the axis of approach to a target in the United
States. However, if we take the whole band of indicated latitudes
in our country, the approach sector for the main and auxiliary
axes will be 70 to 80 degrees.
The possibilities for changing the axes for approach to strike
targets may be significantly increased by launching orbital air-
craft from the air. In this case, the dispersal of launch points
within a radius of 700 to 1000 kilometers will provide for an
average of eight to twelve degrees in the axis of approach to targets
at distances of 10,000 to 15,000 kilometers. If we assume that an
air launch makes it possible to increase combat readiness, viability,
and capability for a surprise attack by orbital aircraft and makes
the fulfilment of assigned tasks more economical, then we may con-
sider that the development of such space weapons systems is a very
good prospect.
However, air launches give rise to new technical and tactical
problems, particularly the need to determine the best launch
points and most favorable flight routes for mother-aircraft, to
define the optimal flight conditions for orbital aircraft with
due consideration to the developing situation, to select cosmo-
dromes for landings, to provide support for landings; and others.
Orbital aircraft also have the capability of widening their
target approach sector by maneuvering along the axis. Their con-
siderable maneuver capability, especially when air launched,
appreciably increases their probability of overcoming enemy anti-
space defenses and assures a wider choice of approach axes to the
target.
Under combat conditions it may not always be expedient to
approach the target from the first orbit. In order to mislead
the enemy regarding their plan of action, orbital aircraft may
be launched ahead of time and not proceed to their target from
the first orbit. There can also be a variant in which an orbital
aircraft is launched with the task of reconnoitering a specific
target but can reconnoiter the entire area during its first orbits
in order to refine the coordinates of the targets which are to be
destroyed by ballistic missiles and space strike vehicles.
For fixed launch points and targets, each orbit has its own
fully defined angles along the main and auxiliary axes of approach
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to the target. Therefore, the approach axis of an orbital air-
craft can be changed depending on which orbit is selected.
In connection with the subject under review, attention
should be drawn to the interesting possibility of making re-
peated approaches to an assigned target without loss of energy
in maneuvering.
This is done in the following manner. At a given orbital
inclination, the trajectories of two selected orbits have one
point of intersection in the Northern Hemisphere and one in the
Southern Hemisphere. This makes it possible to solve the problem
in reverse--to calculate the flight conditions in which the
trajectories of the two selected orbits will intersect at an
assigned point of the target (given a fixed launch point). Re-
peated approaches to the target allow a strike-reconnaissance
space aircraft to complete its target reconnaissance on the first
orbit and to strike the target on the second, or a subsequent,
orbit.
The nature of these conditions for fulfilling combat missions
requires that the flight of a space aircraft be carefully prepared.
The determination of the optimal launch points, the conditions of
flight, and the approach to the target must be completed in a
compressed time period, using electronic computers.
Of considerable importance is the capability of orbital
aircraft to observe the earth's surface and targets on both land
and sea.
The distance at which strike orbital aircraft can spot
ground and sea targets is also of great importance, since it is
this factor which assures that the strike weapons are dropped
on target. For this reason, "space-to-earth" missiles must have
a flight range assuring their reaching the target. In this case,
space aircraft can destroy detected targets, above all, moving
targets, without having to make a second approach.
For fulfilling reconnaissance missions with orbital aircraft
flying in near space areas, it is not always feasible to produce
equipment for surveying a large part of the area of coverage,
since the scale of representation of the terrain will be small
(1:1,000,000 to 1:3,000,000), allowing only a general overall
reconnaissance of broad areas and large targets.
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At the same time, if the aircraft fly at low altitudes and
have equipment to receive large-scale images, it will be possible
to conduct reconnaissance of such Important targets as cosmodromes,
missile launch installations, carrier strike large units and their
deployment, floating bases, elements of the antiaircraft, anti-
missile, and antispace defense systems, etc. The actual area
coverage will be determined by specific reconnaissance equipment
and the feasibility of installing several reconnaissance systems
aboard orbital aircraft.
It must also be borne in mind that in fulfilling reconnais-
sance missions and mounting strikes whose realization demands the
spotting and identification of ground targets, the extent of
terrain coverage is limited by the angle of visibility attainable.
The size of this angle is determined by the capabilities for
interpretation, the distortions in the area and targets under
observation, and the technical characteristics of the observation
equipment.
In working out the problem of the combat use of orbital
aircraft, consideration must be given to the duration of the
observation of ground targets from the space aircraft and to the
time the space aircraft is under observation from ground observa-
tion points.
At a flight altitude of 60 to 150 kilometers, the maximum
duration of observation is three to five minutes. And if we
consider that observation will not begin the moment the target
(space aircraft) comes over the horizon and that the target may
be to one side of the flight path, then the duration of observa-
tion will average 1.5 to 3.0 minutes; this will be reduced by
half when rearward tracking is not available. Although observa-
tion time is thus limited, it is fully adequate for a cosmonaut
to make an observation of the target. As regards transmission
of information from a space aircraft to a command point, obser-
vation time can be significantly increased by an effective
arrangement of receiving stations on our territory.
The, above evaluation of the combat characteristics and
capabilities of orbital aircraft leads to the conclusion that
this type of aerodynamic vehicle is the future delivery vehicle
for nuclear missile weapons and reconnaissance systems. Orbital
aircraft are highly effective for conducting strategic and,
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above all, detailed reconnaissance of land and sea targets in
areas which are inaccessible, or accessible only with difficulty,
to strategic reconnaissance aircraft, such as areas at great
distances or in which there are strong antiair defenses. Orbital
aircraft may in some cases be called upon to perform operational
reconnaissance missions in remote areas of theaters of military
operations. Operational reconnaissance may also be carried out
during regular strategic reconnaissance missions.
To assure rapid action against a newly detected target
discovered during combat operations, orbital reconnaissance must
fulfil its mission in close coordination with strategic strike
weapons--intercontinental ballistic missiles, long-range aircraft,
nuclear submarines, and orbital aircraft.
The choice of a strategic delivery vehicle will be deter-
mined by the nature of the target; its location; the time avail-
able; the condition of enemy antiaircraft, antimissile, and
antispace defense systems; the combat readiness of our strategic
strike means; and other factors. If it becomes necessary to
mount a strike in a compressed period of time, orbital recon-
naissance aircraft may fly in combat formation with orbital strike
aircraft. In this case the mission of the reconnaissance aircraft
will be to designate the target and guide the orbital strike
aircraft to it. Action against targets spotted in coastal zones
may be taken by nuclear submarines using data received from
orbital reconnaissance aircraft.
In view of the maneuverability of orbital aircraft, their
capability for independent actions, and their other combat
features, it may be considered advisable to use them in the
reconnaissance-strike variant as well, in which they will com-
plete their reconnaissance (final reconnaissance) on one of their
first orbits and strike their target on a subsequent orbit.
With their high combat capabilities, orbital aircraft can
successfully fulfil missions for the destruction of nuclear
attack weapons, military-economic targets, and enemy antimissile
and antispace defenses; for combat with carrier strike large
units; and for monitoring the results of actions conducted by
other strategic strike means. The most favorable conditions for
the actions of orbital reconnaissance and strike aircraft will
obviously occur at low space altitudes between 60 and 150 kilo-
meters, especially at altitudes of 90 to 120 kilometers.
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Launching orbital aircraft on a calculated orbit will be the
principal method for assuring that they reach the assigned area.
In all probability, the majority of flights will consist of a
single aircraft or a small group. In mounting massive strikes
in coordination with other types of delivery vehicles, orbital
aircraft will also be able to perform support functions. The
nature of these support functions will be determined by their
place in the overall structure of strategic forces. Thus, in
missions to neutralize antimissile defense systems along the axes
of flight of ballistic missiles, it is advisable to use orbital
aircraft in the first echelon for striking enemy missile defense
elements and, above all, for striking his most forward long-range
observation points.
In addition to reconnaissance and the mounting of strikes,
orbiting aircraft, in coordination with our "earth-to-space" and
"air-to-space" antispace defense systems, can conduct combat with
enemy space vehicles in flight, targets and space areas being
assigned according to altitudes and zones of activity. In this
case, orbital aircraft can carry out combat with enemy space
vehicles at great distances from our territory which appreciably
increases the possibility for using nuclear weapons.
Space interceptor aircraft which are piloted can successfully
identify and intercept space targets, above all those which are
operating at great distances from their own territory, distinguish
the true targets from the false, and monitor the results of the
actions of our other means of destruction of enemy space vehicles.
The presence of a cosmonaut aboard an orbital interceptor
aircraft does not lower the demands for a high degree of automa-
tion of equipment, which must enable the pilot-cosmonaut to fulfil
his functions with a high level of reliability: piloting: identi-
fication and selection of targets; and capture or destruction of
targets. With automated equipment, the pilot-cosmonaut can carry
out various tactical tasks, make the best decisions, use different
types of weapons, depending on the type of target, handle the
capture and removal of space targets if necessary, and rid a space
area of false targets with a small expenditure of power. In order
to increase the duration of their flights, orbital interceptor
aircraft can reach altitudes of 150 to 200 kilometers and carry
out intercepts at altitudes of 700 to 1000 kilometers.
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Declassified in Part - Sanitized Copy Approved for Release 2012/09/26: CIA-RDP10-00105R000100130001-1
Declassified in Part - Sanitized Copy Approved for Release 2012/09/26: CIA-RDP10-00105R000100130001-1 I
-p_m
T-n-P
5
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The solution of the problem of using orbital aircraft in
combat brings to the fore the task of training flight and command
personnel who have already had advanced operational-tactical and
technical training. The strategic nature of the missions to be
carried out, the global scale of the flights, the importance and
complexity of fulfilling combat missions, the great responsibility
of making decisions, the inherent nature of the working conditions
of the crews of space flights, the presence of countless technical
devices and instruments aboard space aircraft--all of these
factors create pressing requirements for training the flight and
command personnel assigned to work with space aircraft.
The use of piloted space aircraft requires the development
of reliable radiation shields ?uar. - s fet of the crew
during space lights. The greatest attention must be given to
the problem of predicting solar flares in the chromosphere, which
can cause a great increase in the natural radiation in areas of
space surrounding the earth. In order to support space aircraft
flights, we must set up a special service to produce reliable
forecasts of the radiation situation in space.
The successful fulfilment
craft ' ? ? - hout resolving the problem of the develop-
ment and establishment of a reliable control system which will
ensure the assignment and monitoring of combat tasks; the collec-
tion, processing, and storage of reconnaissance and other infor-
mation; and the launching and landing of space aircraft. At the
command points, the situation in space must be represented in
graphic form in order that it may be subjected to continuous
evaluation.
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It
?
In conclusion, it should be underlined that orbital and
aerospace aircraft must carry out their combat missions in close
coordination with all other strategic means, as well as with
other types of space vehicles.
The creation of orbital aircraft will mark the beginning
of space aviation, which, with its high combat capabilities,
will further increase the combat might of our Air Forces and of
our Armed Forces as a whole.
T-O-P -C--R-E-T
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50X1-HUM
Declassified in Part - Sanitized Copy Approved for Release 2012/09/26: CIA-RDP10-00105R000100130001-1
OX1-HUM