(UNTITLED)

Document Type: 
Collection: 
Document Number (FOIA) /ESDN (CREST): 
CIA-RDP67B00820R000400040022-4
Release Decision: 
RIPPUB
Original Classification: 
S
Document Page Count: 
2
Document Creation Date: 
December 12, 2016
Document Release Date: 
March 12, 2002
Sequence Number: 
22
Case Number: 
Publication Date: 
October 29, 1964
Content Type: 
CABLE
File: 
AttachmentSize
PDF icon CIA-RDP67B00820R000400040022-4.pdf92.07 KB
Body: 
Approved For Release "002106111. CIA-RDP67B0U820R00n4Q0;A4.?;22-4? 2159Z 29 OCT 64 25X1A ;D%RECSOR 25X1A IRE-CTOR 25X1 A 25X1A S' C R E i T 64 25X1A O C TORE 23172 24 PRIORITY ;.: XCART PRELIMINARY R BAY PACKAGE TEST REPORT. I. GENERAL 1. TYPE I 2. TEST NBR ATF 75B. 3. TEST DATE 23 OCT 64 4. ARTICLE NBR 125 5 TIME T.O. 145524 LAND 1611Z --- I 18380 11 IN 55055 6. PACKAGE OPERATE TIME: 66 MINUTES TOTAL 1509Z AND 606Z. TEST CONDITIONS: A. PRESS ALT 78Mi B. MACH NBR 2.83 C. INS STATUS OK D. WEATHER G CLEAR 8. TEST OBJECTIVES: PRIMARY. OBTAIN STABILIZATION SYSTEM PERFORMANCE WHEN ARTICLE IS OPERATING WITHOUT ENGINE PROBLEMS. S E C R E T onaur t tGwocFGN AiTG. NATIG GGT0G1ALINA [AND DECIJI3SIFICATIGN 25X1A REPRODUGTI N BY OT R THiy THEE !gg tN OFFICE IS PROHIBITED. COPY NO. pprove or Release 200 /6/11 CIA-RD,P67B00820R000400040022-4 Approved For Release 2002/06/11: CIA-RDP67BQ082OR000400040022-4 25X1A S E C R E T 8350 (IN 55055) PAGE TWO JOMPARE V/H DATA WITH ACTUAL FLIGHT PROFILE. COMPARE SC AND DM TAB ?UN INFORMATION 'WITH DATA CHAMBER RECORDS AND PILOTS - RECORDING. SECONDARY. CONFIRM_EXPOSURE PROGRAMMER OPERATES SLIT OVER TOTAL 'LIGHT, TERTIERY. GATHER ADDITIONAL HELIUM CONSUMPTION DATA ,ND ATMOSPHERIC SCATTER DATA. 9. TEST RESULTS: STABILIZATION INFORMATION IS NOT CONSIDERED 'ALID DUE TO PROBLEMS ENCOUNTERED BY PILOT WITH ENGINES. Ht:CAUSED ROUGH FLIGHT WITH MANY OSCILLATIONS AND PERTURBATIONS* N LANDING APPROACH PITCH DOWN ATTITUDE APPARENTLY KEPT SYSTEM CAGED 'OR LAST PART OF FLIGHT. THERE IS VERY POOR CORROLATION ?ETWEEN DATA CHAMBER READOUT AND SC AND DM RECORD. POSITION, V/H ND GROUND SPEED DO NOT COINCIDE BETWEEN. THE TWO SYSTEMS? THE SLIT ROGRAMMER OPERATED THROUGHOUT THE WHOLE FLIGHT CONTROLLING THE ;L ITS. THE FAIL LIGHT ON THE PANIC PANEL STAYED ON DURING THE TIME THE SYSTEM WAS IN STANDBY, BUT WENT OUT IN OPERATE. THE ELt M CONSUMPTION WAS ABOUT 5.7 GMS PER MINUTE. ATMOSPHERIC ATTER? DATA WAS TAKEN. END OF MESSAGE S E C R E T Approved For Release 2002/06/11: CIA-RDP67B0082OR000400040022-4