AERODYNAMIC VEHICLE ACTIVITY KAPUSTIN YAR CRUISE TEST COMPLEX D SITE 1, USSR 17 MAY 1982
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Collection:
Document Number (FOIA) /ESDN (CREST):
CIA-RDP90T00784R000100240004-5
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RIPPUB
Original Classification:
S
Document Page Count:
5
Document Creation Date:
December 28, 2016
Document Release Date:
September 9, 2011
Sequence Number:
4
Case Number:
Publication Date:
June 11, 1982
Content Type:
REPORT
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CIA-RDP90T00784R000100240004-5.pdf | 143.06 KB |
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NOFORN
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CONTROL NO. Z-15234,/82
'NPIC/IEG (6/82)
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(c) NATIONAL PHOTOGRAPHIC INTERPRETATION CENTER
Page 1 of 2 Attachment to Z-15239/82
Copy NPIC/IEG (6/82)
11 JUNE 1982
AERODYNAMIC VEHICLE ACTIVITY
KAPUSTIN YAR CRUISE TEST COMPLEX D SITE.1, USSR
j, (S/D) SIGNIFICANCE: ACTIVITY INVOLVING TWO AERODYNAMIC
VEHICLE (ADV) SYSTEMS CURRENTLY UNDER DEVELOPMENT WAS OBSERVED.
2. (S/D) REMARKS: ADV-4 CONFIGURATION CONFIRMED.
(S/D) AN ADV-4 WAS ON A DOLLY ON THE LOOP ROAD NORTH OF LAUNCH
PAD D-3. THE ADV-4 IS A SMALL GROUND-LAUNCHED AERODYNAMIC
VEHICLE WHICH HAS BEEN UNDERGOING TESTING AT KAPUSTIN YAR SINCE
1 9 7 8 . THE FUSELAGE OF THE ADV-4 IS 3 . 0 METERS LON 9 X1
THE LEADING EDGE OF THE MID-MOUNTED MAIN 25X1
WING FROM THE NOSE. THE WING HAS A SLIGHTLY 25X1
TAPERED LEADING EDGE, A STRAIGHT TRAILING E 25X1
LORI
THE HORIZONTAL STABILIZER ALSO APPEARED TO HAVE A 25X1
TAPERED LEADING EDGE AND A SPAN THE 25X1
CONFIGURATION OF THE VERTICAL STABILIZER AND ENGINE WAS NOT
DISCERNIBLE. AN ADV-4 TRANSPORTER-ERECTOR-LAUNCHER (TEL) WAS
ALSO ON THE LOOP ROAD, APPROXIMATELY 20 METERS WEST OF THE
ADV-4. A SECOND ADV-4 TEL WAS IN THE OPERATIONS AREA OF SITE 1.
(S/D) THE ROLE OF THE ADV-4 IS STILL UNKNOWN. THE SIZE OF THE
ADV-4 AND ITS ASSOCIATION WITH A TRACKED TEL MAY INDICATE THAT
THIS VEHICLE WILL BE USED AS A HIGHLY MOBILE, SHORT-RANGE
BATTLEFIELD RECONNAISSANCE DRONE.
(S/D) TWO ADV-2, FOUR ADV-2 LAUNCHERS, AN ADV-2 TRANSPORTER,
AND A PROBABLE ADV-2 SOLID ROCKET MOTOR BOOSTER WERE OBSERVED
AT SITE 3. THE TWO ORIGINAL LAUNCHERS WERE IN
FIRING POSITION ON PAD D-3. THE OTHER TWO LAUNCHERS, WHICH
WERE PARKED IMMEDIATELY NORTH OF PAD D-3, WERE OF THE NEW
11.4-METER CONFIGURATION. ONE WAS OCCUPIED BY A FULLY
ASSEMBLED ADV-2C. THE OTHER WAS ATTACHED TO A KRAZ 214 PRIME
MOVER, CONFIRMING THAT THESE LAUNCHERS ARE TOWED AND NOT
These notes have been prepared for briefing purposes only and should not be used for detailed ana-
lytical work. Their use should be restricted to the particular briefing board(s) they were prepared for
and must be considered valid only for the reporting period as indicated by the date of issue.
WARNING NOTICE
Intelligence Sources
and Methods Involved
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SELF-PROPELLED. THE FIRST OF THESE NEW LAUNCHERS HAS BEEN
THE SECOND WAS FIRST OBSERVED ON
A PARTIALLY ASSEMBLED ADV-2 AIRFRAME WAS ALSO
ON PAD D-3 AND A PROBABLE ADV-2 SOLID ROCKET MOTOR BOOSTER WAS
(c) NATIONAL PHOTOGRAPHIC INTERPRETATION CENTER
ADJACENT TO A TRUCK-MOUNTED CRANE. THE PROBABLE BOOSTER
2rX1
25X1
SOLID ROCKET MOTOR BOOSTER IS PROBABLY USED TO ASSIST IN
LAUNCHING THE TURBOJET/TURBOFAN-POWERED ADV-2, A FEATURE
PREVIOUSLY OBSERVED ON THE SOVIET DR-1 GROUND-LAUNCHED TARGET
DRONE.
Page _2 of 2
Copy
Attachment to Z-15239/82
A 25X1
(S/D) THE ADV-2 IS A GROUND-LAUNCHED CRUISE VEHICLE ON WHICH
TESTING BEGAN AT KAPUSTIN YAR IN 1975. SINCE THE
IDENTIFICATION OF THE FIRST LAUNCHER, THE LEVEL OF 25X1
ADV-2 ASSOCIATED ACTIVITY HAS INCREASED, PROBABLY INDICATING
THAT A NEW TEST PHASE OF THE ADV-2 IS UNDERWAY. THE ACTUAL
ROLE OF THE ADV-2 STILL REMAINS UNKNOWN. 25X1
These notes have been prepared for briefing purposes only and should not be used for detailed ana-
lytical work. Their use should be restricted to the particular briefing board(s) they were prepared for
and must be considered valid only for the reporting period as indicated by the date of issue.
WARNING NOTICE
Intelligence Sources
and Methods Involved
NOFORI\
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3. (S)