ATIC BULLETIN AEROSPACE TECHNICAL INTELLIGENCE CENTER

• Document Type: CREST
• Collection: General CIA Records
• Document Number (FOIA) /ESDN (CREST): CIA-RDP78-03642A001200060016-5
• Release Decision: RIPPUB
• Original Classification: S
• Document Page Count: 14
• Document Creation Date: December 22, 2016
• Document Release Date: May 24, 2011
• Sequence Number: 16
• Publication Date: March 17, 1961
• Content Type: REPORT

Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642AO01200060016-5
cc F Fr ~S
ATIC BULLETIN
AEROSPACE TECHNICAL INTELLIGENCE CENTER
WRIGHT- PATTERSON AIR FORCE BASE, OHIO
VOLUME X NUMBER 7
17 MARCH 1961
This document is releasable to officially sponsored
r pnsontativos of the U.K., Canadian, Australian,
and New Zealand Governments In accordance with
AF-DCMI.
Copy No. ~`*
T61-0007
Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642AO01200060016-5
 Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642AO01200060016-5
SECRET
A T I C B U L L E T I N
TABLE OF CONTENTS
Vol X, Nr 7
17 March 1961
Editor Associate Editor
Mr. Lee H. Strahl MSgt Earle F. Gilmore
Page
1 (U) Guidance Systems for Soviet Air-To-Surface Missiles 3
Mr. D. D. Notestine
2 (U) New, High-Performance Soviet Gliders
Mr. J. L. Rohn
3 (U) Soviet VLF Navigation System
Mr. L. S. Peterson
(U) Electric Explosions in the USSR 8
Maj P. J. Wolf
NOTE
The ATIC ULLETIN is,published every Friday by he AerQ ce Technical Intelligence
Center Wr+ght-- atterson Air Force Base, Ohlo, to furni intelligence information qn dive -
optnen s elate to the technology of fgreigi ai r power - inttorMation that is timely and reason
ably authentic but not necessarily confirmed.
It Is uggested that this Center be consulted before specific use is made of the information
contained in any Item that is published herein.
nfo tioi conflicting with pertinently of cling that e~nrofned fin is publication should
~e forwa ed by the recipient directly to the Commander, Aerospace echnic~aoI Intelligence
ter. his i no obrpgate} or of rs respgnsibillty far sending uch info~matio or y
pertinent Intelligence tiara through already established intelligence collection channels of the
various services or agencies of the US govbmment.
WARNING: This documents rains informatio ~of~ c}ingthe nati aI defe se of d1 United
States within the meaningof thesplonoge Law, Title 18, U.S.C., Sections 7'93 an94. Its
transmission or the revelation o ifs contents in any manner to an unauthorized person is pro-
hibited by law.
T61-0007
SECRET
Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642AO01200060016-5
 Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642A001200060016-5
SECRET
1. (U) GUIDANCE SYSTEMS FOR SOVIET AIR-TO-SURFACE MISSILES
Mr,. D. D. Note Stine
ATIC has estimated the guidance-system characteristics and capabilities
of Soviet air-to-surface missiles having ranges of 55, 100, 350, and 500-1000
NM. The estimates are based on information from all available sources,
known mission requirements, and established Soviet practices.
The guidance system estimates for the various classes of air-to-surface
missiles are shown in Table I on page 4.
Equipment Descriptions
(1) Beam Rider with Semi-Active Radar Homing.
A beam rider with semi-active radar homing guidance system is
estimated for the 55-NM air-to-surface missile. The missile rides
a radar beam for the first two-thirds of its flight, and then with semi-
active radar homes on the target. The control switches when the field
strength of the received echo from the target reaches a pre-set value.
A pulsed X-band radar in the launching aircraft provides both the
energy for beam-riding and target illumination for semi-active homing.
Thus, it is necessary that the radar beam be directed at the target
throughout the missile flight.
(2)
Inertial Guidance With Active Radar Homing.
An inertial. guidance system is estimated for the 100 and 350-NM
air-to-surface missiles used against stationary targets. For strikes
against ships at sea, an active radar will also be employed in the mis-
sile for terminal guidance to the target.
The navigation system of the launching aircraft aligns the inertial
equipment and provides initial position to the guidance computer prior
to launch.. After launch, the computer integrates acceleration data
from the inertial equipment to determine missile position. Computed
values are then compared with programmed target data to obtain
guidance signals for the flight-control system.
When terminal homing is used against ship targets, the active
radar locks on the target and takes over guidance of the missile.
The missile-borne radar is estimated to be capable of target ac-
quisition at 50-NM range against a 100-square-meter ship target.
-3- T61-0007
SECRET
Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642A001200060016-5
 Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642AO01200060016-5
Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642AO01200060016-5
 Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642A001200060016-5
SECRET
2. (U) NEW, HIGH-PERFORMANCE SOVIET-GLIDERS
Mr. J. L. Rohn
During 1960 a number of Soviet publications revealed the existence of a
new, high-performance Soviet glider. This single-seat all-metal glider
reportedly was constructed under the supervision of the renowned aircraft
designer O. K. Antonov and it reflects a high degree of aerodynamic refine-
ment. It is designated the A-15.
Sport-type gliders normally have little military or intelligence value,
but this is the third significant glider development by the Antonov Design
Bureau in as many years and indicates the advanced capability of the design
bureau. Statements such as "The world's sportsmen have never seen such
gliders as the A-15" (by test pilot S. A. Anokhin, who has flown gliders for
over thirty years) have been published. Moreover, the data released on the
A-15 discloses that lift/drag ratios have been improved to the extent that the
developments probably will be applied to larger aircraft.
On 6 May 1960, a Moscow broadcast stated that the A-15 has a glide
ratio of 42 to one. Since the glide ratio of a glider directly indicates the
lift/drag ratio, this value of 42 for the A-15 glider is exceptional. The
glide ratio of the best high-performance gliders has been between 25-32
when the lift had been improved and the drag reduced as much as practica-
ble. On one design, however, the late Dr. August Raspet of Mississippi
State College achieved a glide ratio of .55 through a remarkable effort in the
reduction of drag, utilization of a laminar-flow airfoil, and employment of
boundary-layer control. Thus, the glide ratio on the A-15 glider is consid-
erably better than all previous glider designs, other than the one outstanding
effort, and it probably was achieved by methods similar to Raspet's.
It became evident that the glide ratio claimed is approximately correct
when it was announced that the A-15 glider had established two new World
Records. The Moscow News, on 22 June 1960, said that the A-15 has been
flown around a triangular closed course of 100 km at an average speed of
111. 388 kmh (60 knots). This speed surpasses the 1959 US.record of
107.040 kmh, the Yugoslavian record of 97. 066 kmh and the USSR record of
77. 144 kmh. The flight was made by Mikhail Veretennikov in May 1960. He
was towed by a Yak-14 (CROW) light transport to 700-800 meters (8200 ft)
altitude, and flew from Suma City to Ulyanovka to Mikhylovka and back to
Suma. In June 1960, the same pilot and glider made a 714 km (385 NM)
"goal" flight (flight to a pre-determined destination) in eight hours, better-
ing the 1956 French record by 23 km.
In October, Isvestia disclosed that the A-15 had a "remote pilot system."
This system is identified as a two-way radio (transceiver) having a range of
90 km (almost 50 NM), which operates with a responder beacon. The system
uses coded signals from a ground radar and from the aircraft response
-5- T61-0007
SECRET
V
Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642A001200060016-5
 Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642AO01200060016-5
SECRET
the location, distance, altitude, and speed of the glider can be determined.
This transceiver reportedly was especially developed for this glider, be-
cause available sets weighed 30-40 kg (66-88 lb). It uses "rod tubes".
developed by Andeyev, a corresponding member of the USSR Academy of
Sciences; these tubes are said to be economical, light, small, and able to
withstand high overload and vibration.
The oxygen system of the A-15 is a standard Soviet aircraft system
having a two-liter tank with 150-atmosphere pressure; it is effective to an
altitude of 12, 000 meters (40, 000 ft). A water ballast system, ? comprising
two 25-liter (6.6 US gal) tanks in the wings, permits the glider to fly faster
under strong lift conditions; during weak-lift conditions the water can be
jettisonned to obtain a lower wing-loading. The glider is also equipped with
a retractable undercarriage, airbrakes and a "thermo-visor" to assist the
pilot in locating upward-moving air currents.
The same design bureau previously had developed the two-place A-11
and the single-place A-13 glider designs (see ATIC BULLETIN, 30 May 58,
Item 3). Both of these were also of,all-metal construction, and production
was initiated in mid-1958 under contract to the DOSAAF Central Committee.
The two were identical except for the seating and the wing unit, the A-11
having a larger span designed for long-distance flights'and the A-13 having
a somewhat smaller span more suitable for aerobatics. The Soviet news-
paper "Pravda Ukrainy" (22 June 1958) reported that both gliders were
designed and constructed under the supervision of A. Yu. Monotskov from
the design office of O. K. Antonov. (One Alexander Yurievich Monotskov
attained recognition in 1954 when he modified one of Antonov's A-9 gliders
into the flapping-wing "Kashuk"). According to one report both the A-il
and A-13 are stable and are exceptionally maneuverable gliders. Both
are described as cantilever, mid-wing monoplanes with tapered wings hav-
ing a single main spar and auxiliary front spar. Both versions have "plate
brakes, " reinforced skin fuselages, V-tails, and single-wheel retractable
landing gear aided by a skid. The A-11 also has lift flaps.
Following is the available technical data concerning the A-11, the A-13
and the A-15.
Wing Span
Length
Wing area
Net weight
Gross weight
Wing loading 33 *ksm ( 78 psf) 35
16.5 m ( 55 ft) 12.1 m ( 40 ft) 17 m 56 1ft
6 m ( 20 ft) 6 m 20 ft) 7 in 23 ~ft~
12.15 m2 130 ft2) 10.44 m2 112 ft2). - - - - - - -
310 kg 680 lb) 270 kg (600 lb - - - - -
400 kg (880 lb) 360 kg (800 lb) 400 kg (880 lb)
Towing speed - - - - - - - - - - 250
Max dive speed 300 kmh (162 kn) 400
*Kilograms per square meter.
SECRET
*ksm 82 psf)
kmh 135 kn) - - - - - - r-
kmh (215 kn) 250 kmh (1.35 kn)
Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642AO01200060016-5
 Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642A001200060016-5
SECRET
Attesting to the quality of these newer gliders, an A-10 (two-place
version of the A-9) set a World Record for a goal flight on the same day
that the A-15 set the single-place goal flight record. The A-10 with a
passenger aboard, flew 600 km (325 NM) which was 58 km more than the
previous record set by a Polish pilot, but more than 100 km less than the
A-15 single-place record flight. (AFCIN-4F2) (The over-all classification
of this item is CONFIDENTIAL.) (Releasable to UK, Can, Aus, NZ, and
NATO.)
3. (U) SOVIET VLF NAVIGATION SYSTEM
Mr. L. S. Peterson
Preliminary analysis of recent Soviet VLF signals indicates that a new
navigation system is in the early stages of development. The signals originate
from three separate 10 to 15-kc transmitters located in the southwest part of
the Soviet Union; the signals are sporadic and unstable. ATIC previously
believed that the signals were sufficiently stable to be used as a. VLF hyper-
bolic navigation system, similar to one being developed in the US. The 10 to
15-kc signals from the three existing transmitters must be stable and phase-
locked to position accurately missiles or missile-launching, submarines or
aircraft. Signals emanating from phase-locked systems can provide naviga-
tion fixes accurate to within ?1 NM at ranges of 5000 NM.
Until these signals exhibit stable characteristics, this cannot be consid-
ered an effective navigation. system. (AFCIN-4E1) (The over-all classifica-
tion of this item is SECRET.) (Releasable to UK, Can, Aus, NZ, and NATO.)
SECRET
Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642A001200060016-5
 Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642A001200060016-5
SECRET
(U) ELECTRIC EXPLOSIONS IN THE USSR
Maj P. J. Wolf
Electric explosions, underwater lightning, and electrohydraulic effect,
are all Soviet terms for the same phenomenon. While it is endless in applica-
tion, in essence it is simple, consisting of the discharge of a large, high volt-
age electrical current between two electrodes through a thin wire or through a
fluid. When such discharge occurs, it results in a brilliant flash of light, a
loud noise, and a shock wave of considerable magnitude, which can be har-
nessed to do useful work. It also radiates heat, light, electromagnetic waves,
X-rays, and possibly other forms of radiation,.
In behavior and effect, it is very much like the detonation of explosives,
but it can be better controlled and manipulated.
While some electrical discharges such as.occur in lightning or a spark
plug are quite common, it is difficult to conceive the magnitude of the reac-
tion when large amounts of energy are pumped through a restricted channel
in a brief period of time. It may be helpful to consider that one discharge at
a US facility produced pumping energy at the rate of 22, 000, 000 horsepower.
This was accomplished by pumping up a large capacitor bank (200 capacitors
at 7 1/2 micro-farads each) to 20, 000 volts and suddenly discharging the
stored energy in 10 millionths of a second. When such a discharge is passed
through a thin wire in air, the wire is instantly vaporized in a brillant flash
and with a loud report. In water, the shock is considerably intensified, pos-
sibly because the plasma channel that is formed cannot expand fast enough due
to the relative incompressibility of water. This results in much higher tem-
peratures and pressures. Some idea of the severity of the shock can be de-
duced from the fact that an open-topped tank of water weighing ten tons jumps
six inches off the floor every time a discharge is made within it.
Credit for the practical exploitation of this phenomenon apparently belongs
to Lev Yutkin of Leningrad Polytechnic Institute who was discussed in the
article that triggered ATIC's interest in this field in mid-1958. The article
discussed a new rock crushing process, but it was apparent that the shock
waves developed might be even a better way of forming of space age materials
than explosive forming, which was then a much discussed idea. A search of
available information soon showed that Yutkin had been active in this field
since his student days in 1938, when he accidentally. shattered a vessel while
experimenting with high voltage currents. In 1955, he published a book which
listed some 150 practical applications and discussed in detail the following
salient points:
(1) The basic concept and arrangement of the apparatus.
T61-0007 -8-
S E C R E T
Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642A001200060016-5
 Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642A001200060016-5
SECRET
(2) The limitations of the process.
(3) Applications in such diverse fields as the forming of metals,
pumping of liquids, propulsion devices, surface hardening of metals,
production of fine metal powders, unusual chemical reactions, and
many more.
(4) The existence of a compact practical means of repetitive
shocking.
One of Yutkin's earliest applications was a rock drill with phenomenal
performance. It allegedly could bore a 1 1/2-inch hole 50 feet into solid
rock in one hour using 650 watts of power. While rock drills are of little
consequence to air weapons, they supply evidence of the ability to produce
a continuing succession of electrical shocks.
Further study of this subject shows that the Soviets applied their
repetitive shocking capability to drive an extrusion press prior to 1958.
In 1960, a patent was issued for presses up to 100, 000 tons using this
principle. The largest US extrusion press is 14, 000 tons and uses regular
hydraulic pumps. The press covered in the Soviet patent is stated to be
for the production of one piece, "internally ribbed tubes, " suggestive of
Titan-type structures. The size of the tubes is not specified, but if such
a 100,000-ton press does exist, it would be easily capable of producing "tubes
large enough for ICBMs. The persons associated with this Soviet patent are
high level, technically competent individuals.
The Soviets have apparently found many other practical applications for
this phenomenon; among these are metal forming, heat treatment, high pres-
sure pumping for liquids and liquid metals, and novel chemical reactions.
The latter is illustrated by the fact that an electrical discharge between
electrodes placed in a container filled with kerosene will precipitate elemen-
tal carbon out of the hydrocarbon molecules. The process is also used to
produce improved polymers.
The story of Yutkin seems to be one of a practical experimenter with an
obsession about using electrical energy to do work directly, rather than ap-
plying it through relatively inefficient electric motors, magnets, or other
transducers. He apparently worked for years at LPI, essentially unnoticed
and probably on a minimum budget, developing a number of successful ap-
plications for his idea. These developments have been picked up by such
prominent organizations as Tsniitmash (Central Scientific Institute for
Technology and Machine Building) and after pilot plant tryouts designed into
usable production equipment.
Yutkin also attracted the attention of the Academy of Sciences in 1955,
when one of the members reviewed his work, praised him highly, and pre-
dicted a great future for this field. Literature concerning this leaves the
-9- T61-0007
SECRET
Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642A001200060016-5
 Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642AO01200060016-5
SECRET
impression that the Academy judged this work to have such merit that it
warranted a broad program of research by high level scientists aimed at
understanding and further exploiting the phenomenon.
From this point in time, prominent physicists started doing research
in this field. Among the better known are the following:
(1) Dr. Peter L. Kapitza -- Head of the Institute of Physical
Problems, Moscow.
(4) Major General G. I. Pokrovsky -- Physicist, active in Soviet
missile and space program.
(3) Dr. G. I. Babat -- Head of the Institute of Energetics, Moscow.
(4) Dr. K. P. Stanyukovich -- Head of Mathematics, MVTU.
(5) A. S. Zingerman -- Chair of Electro Technology, Institute of
Civil Engineers.
It is obvious from the positions and backgrounds of these people, as well'
as from the nature of their research, that their efforts are not directed at
metal-working problems. Instead, it would appear that a group of high
caliber scientists who are associated in various ways with missile and space
activity are working on a coordinated program involving the electrohydraulic
effect, ball lightning, and magneto gas dynamics. Kapitza and Babat have
both been extremely interested in ball lightning and are rumored to be work-
ing on a missile defense system involving the electrohydraulic effect. Yutkin
is alleged to have developed a ball lightning projector in his laboratory. It'
could be most significant that Babat was "accidentally killed" while
Khrushchev was in the US intent on producing some technological surprise
which fizzled. No further details on Babat's death were given. Rocket
Marshal Nedelin was also "accidentally killed" during the same week.
Very little information is available on Soviet weapons applications of this
phenomenon; for this reason, some US unclassified work was reviewed to ob-
tain clues to the ultimate Soviet applications. The review presents a picture
in the US very similar to Yutkin's earliest years, with minimum budgets and,
in some cases, bootleg research. Much of the current US effort stems from
a report on Soviet activity made to some segments of US industry by ATIC in
November, 1958.
Despite a late start and a low level of effort, the US has now developed
the process to a point where air weapon hardware can be formed by electric
explosions. Most of the applications the Soviets have mentioned, however,
remain unexplored. The three principal companies involved are Convair,
Ft. Worth; Chrysler Missile Division; and Republic Aviation Corporation.
T61-0007 -10-
SECRET
Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642AO01200060016-5
 Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642A001200060016-5
SECRET
Some US work was accomplished by isolated researchers, but it was of the
small (1/2 inch) exploding wire type, and it had little practical application.
(Chrysler can now explode 40 feet of wire in one shot and has formed a 42-
inch-diameter missile bulkhead.)
In formulating probable Soviet applications of this process, US industrial
thinking was used as a guide. With metal working already established,
thoughts are now being given to other industrial and chemical applications.
Other possibilities are long range sonar for submarine detection and possibly
propulsion systems. Also being considered are destructive devices of vari-
ous sorts. Chrysler claims to have vaporized a beer can at a moderate
distance from the power source and also to have vaporized a rifle bullet
traveling at 3000 ft/sec.
In summary, thanks to Yutkin, the Soviets have led for some time in
practical applications of the electrohydraulic effect. It appears that this
phenomenon has received continuing high level Soviet scientific attention
since 1955 and that results commensurate with that effort can be expected.
Probably their early development of a means of repetitive shocking.opened
up many more fruitful areas of research than. was the case in the US. , On
the other hand, US effort has been limited, but has demonstrated that this
phenomenon can be harnessed for useful and sometimes startling results.
(AFCIN-4E2) (The over-all classification of this item is SECRET.) (Re-
leasable to UK, Can, Aus, and NZ.)
-11- T61-0007
SECRET
Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642A001200060016-5
 Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642AO01200060016-5
SECRET
SECRET
Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642AO01200060016-5
 Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642AO01200060016-5
SECRET
AFCIN
AFCIN-M
ADC 2
CINCONAD 1
PACAF
PFIDC-SD
17
Govt Agencies
AEC
1
AFCIN-P
SDC 1
SAC D/I
1
ANPO
1
AFCIN-lA
TAC
4
ARPA
1
AFCIN-1B1
AMC
USAFE
CIA
23
AFCIN-1C3
BNWGR-CD 1
ELINT Proces. Cen
7
JCS/J-2
1
AFCIN-1D
EDSD
1
AF Security Ser
NASA
1
AFCIN-lE-OS-GDR
LMBM
1
ACSCC
2
Ames Cen
1
AFCIN-2
LMEG
1
AFSSOP
2
Langley Lab
1
AFCIN-2A
LMG
1
6922 Radio Gp (M)
1
Lewis Lab
1
AFCIN-2B
LMR
1
NSA-CREF-212
12
AFCIN-3D2
MCF
1
USAF AirA
AFCIN-3D4
MCG
1
Bulgaria
1
USLO/SACLANT
1
AFCIN-3F
MCMT
1
Canada
1
USMIC/SG (NATO)
1
AFCIN-3F1
MCP
1
Czechoslovakia
2
USNMR/SHAPE
2
AFCIN-3F2
MCT
1
England
1
AFCIN-3F4
MCW
1
Liaison,O/London
1
Field Offices
AFCIN-3H1
MOAMA
1
France
1
Det Nr 2
2
AFCIN-3H2
MOAMA
1
ALO Hong Kong
1
DetNr 3
6
AFCIN-31 (ARD)
OCAMA
1
Hungary
1
Det Nr 4
1
AFCIN-3K1
OOAMA
1
Italy
1
AFCIN-3K2
RCG
15
Japan
1
AJSS
AFCIN-3K3
SBAMA
2
Poland
1
BDSW
AFCIN-3R1
SBAMA
1
Rumania
1
CJS
AFCIN-3R2
SMAMA
1
Sweden
1
RNZAF
AFCIN-3W1
WRAMA
1
Switzerland
1
AFCIN-3W2
2710th
AB Wing
1
Taiwan
1
AFCIN-3W3
Turkey
1
ACIC
ARDC
7
USSR
1
AEDC
1
Hq USAF
AFBMD
2
Army
64
AFCCS
2
AFCCDD
4
Dept of State
5
AFCRM-A (Norton)
1
AFCRL
6
Navy (ONI)
15
AFCSA
1
AFFTC
1
OASD/C (SSC)
1
AFDAP-R (RAND)
2
AFMTC
(Hol)
3
OASD (DD R&E)
2
AFDAP-W
2
AFMTC
1
OASD/ISA
1
AFDDC
1
AFRD
2
OASD (PA)/OSR
1
AFDDC-PA
7
AFSWC
1
AFMTC
2
APGC
1
Joint Commands
AFOOP-CP
1
RADC
6
CINCAL
1
AFOOP-SA
1
WADD
39
CINCLANT
1
C
LM
AFOOP-SV-ES
1
CIN
NE
1
AF1AC
1
Air Trng Comd
CINCPAC J-2
1
AFXPD-PL-FP
1
Sheppard AFB 5
COMUSTDC
1
P
1
USCINCEUR
1
AFXPD-PL-S
AFXPD-PL-WP
1
AAIRC 2
Committees
SAFRD
1
AU Library 1
GMAIC
1
Alt Hq
3
CONAC 1
JIC
1
AJCC
3
MATS 4
WSEG
4
NOTE: Requests for
Intelligence
this publication should be directed to the Aerospace Technical
Center, Wright-Patterson Air Force Base, Ohio., ATTN: AFCIN-4.
SECRET
Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642AO01200060016-5
 Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642AO01200060016-5
SECRET
SECRET
Sanitized Copy Approved for Release 2011/10/19: CIA-RDP78-03642AO01200060016-5