U2R PHOTO CHART REPORT

Document Type: 
Collection: 
Document Number (FOIA) /ESDN (CREST): 
CIA-RDP33-02415A000100080007-4
Release Decision: 
RIPPUB
Original Classification: 
K
Document Page Count: 
15
Document Creation Date: 
December 16, 2016
Document Release Date: 
August 5, 2004
Sequence Number: 
7
Case Number: 
Content Type: 
CHART
File: 
AttachmentSize
PDF icon CIA-RDP33-02415A000100080007-4.pdf1.56 MB
Body: 
Approved For Release 2004/08/31 : CIA-RDP33-02415A00010008000 -4 SP 978 k- l U-2R PHOTO CHART REPORT NRO and USAF review(s) completed. Approved For Release 2004/08/31 : CIA-RDP33-02415A000100080007-4 Approved For Release 2004/08/31 : CIA-RDP33-02415A000100080007-4 Approved For Release 2004/08/31 : CIA-RDP33-02415A000100080007-4 ? ? ?i ? i ? - ? ? ? ? ? ? - i i A Approved For Release 2004/08/31 : CIA-RDP33-02415A000100080007-4 m - - m ? m ? ? ? ? ? ? ? ? - IM - Approved For Release 2004/08/31 : CIA-RDP33-02415A000100080007-4 IM _ ^_ C O m ? Gi _ _ _ _i Approved For Release 2004/08/31 : CIA-RDP33-02415A000100080007-4 U2R INBOARD P "B"CAMERA rP$W J-75 P-13B ENGINE REMOVABLE NOSE PAYLOAD AREA COCKPIT "Q BAY N'M BAY TAIL BREAK FS 608 ? - - - - - - - - - - - - - - - - - m Approved For Release 2004/08/31 : CIA-RDP33-02415A000100080007-4 INTERNAL VOLUME COMPARISO U-2R E U 2C 4 INCHES AVERAGE INCREASE IN COCKPIT DEPTH ? i - ? i ? ? ? ? ? O m Approved For Release 2004/08/31 : CIA-RDP33-02415A000100080007-4 U2R PILOTS INSTRUMENT PA! - - - - - - - - - - - - - - - - - - - Approved For Release 2004/08/31 : CIA-RDP33-02415A000100080007-4 QUICK CHANGE PAYLOAD Ct UPPER'E"8AY HATCH UPPER HATCH WBAY REMONAME NOSE LATCHES .4 ?4AT04 LAIIYEROQ"BAY HATCH Approved For Release 2004/08/31 : CIA-RDP33-02415A000100080007-4 Approved For Release 2004/08/31 : CIA-RDP33-02415A000100080007-4 IM IM IM Approved For Release 2004/08/31 : CIA-RDP33-02415A000100080007-4 G - - Approved For Release 2004/08/31 : CIA-RDP33-02415A000100080007-4 U-2 R NORMAL FUEL 5X1 NORMAL OVERLOAD (CURRENT) TAKE-0FF WEIGHT 30,130 34750 24,780 ZERO FUEL Wt . 17,400 17,400 14-8600 Approved For Release 2004/08/31 : CIA-RDP33-02415A000100080007-4 MAX. ALTITUDE- LOITER II HRS. QMIN- @ 64,800 ALTITUDf ^_ _i _ _ m ~ _ _ m _ m _ _ m m ~ Approved For Release 2004/08/31 : CIA-RDP33-02415A000100080007-4 r `^ - r - - - - - - Iii r Approved For Release 2004/08/31 : CIA-RDP33-02415A000100080007-4 U 2R MINIMUM DEVELOPMEP EXPERIENCE 11 PERFORMANCE AND FLYING QUALITIES UJ2R IS Y3 SCALED UP VERSION OF BASIC U-2. xr.F! WING ASPECT RATIO AND THICKNESS RATIO ARE UNCHANGED. PERFORMANCE BASED ON OVER 100,000, HOURS GF *2 FLIGHT TIME. IMPROVED LONGITUDINAL TRIM WITH ALL MOVING HORIZONTAL STABILIZER. 7I ` '. I IGURATION CHANGES IN-CM''- TO IMPROV RESENT U-2 FLYING QUALITIES I 8 d il " is ? NO TECHNICAL BREAKTHROUGHS REQUIRED IN THE AIRFRAME OR ENGINE. 12 r Approved For Release 2004/08/31 : CIA-RDP33-02415A000100080007-4 2R MINIMUM DEVELOPMENT WITH MAXIP EXPERIENCE STRUCTURE AND-...WEIGHT STRUCTURAL CRITERIA N H E ` ~! R 11 4 STRUCTURAL ARRANGEMENT ESSENTIALI~Y.'HE . r SAME AS THE BASIC U-2 LOAD AND STRESS ANALYSES PROVEN BY.UV~R . 100,000 HOURS OF U-2 FLIGHT TIMEy CONVENTIONAL ALUMINUM ALLOYS USED THROUGHOUT. WEIGHT ESTIMATE IS CONVENTIONAL EXTENSION OF ACTUAL U-2 WEIGHTS. 13