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AVIATION: (Airforce tests supersonic Issue Number B=ll X-2) 7479x2 Subject Cameraman ROCKET BELL X-2 UNVEILED FOX(DD) Length Neg. Dupe Pos. Cuts BK NO: 6960-8 290ft. FG DUPE caption junked a Can No. tor card made Description and Remarks MISC. USA: (ext.view of the Date of EAugust 1955 USAF BELL X-2 on the ground--plane being attached to "mother" B-50--B-50 taxis,taking off and in flight--"mother"plane drops the X-2 and it glides to ground (not using power at all,Just gliding)--landing, coming to halt on skis INFORMATION: (This successor to the K-1A--It was built to probe the thermal barrier,as a flying research laboratory--to investigate probéems beyond the speed sound ans to surpass speed of 1650 MPH-- "mother"plane carries vehicle to specified altitude where it begins its flight on its own power--th conserves fuel and power for longer flight--skis replace wheeis to fu: ther reduce weight to aid speed--built by Bell Aircraft in conjuntion SEE OVER PRINTED IN U.S.A. FORM 2530-8M-12/68 OVER

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Page context
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    "ocrText": "AVIATION: (Airforce tests supersonic\nIssue Number\nB=ll X-2)\n7479x2\nSubject\nCameraman\nROCKET BELL X-2\nUNVEILED\nFOX(DD)\nLength\nNeg.\nDupe\nPos.\nCuts\nBK NO: 6960-8\n290ft.\nFG DUPE\ncaption junked a\nCan No.\ntor card made\nDescription and Remarks\nMISC. USA: (ext.view of the\nDate of EAugust 1955\nUSAF BELL X-2 on the ground--plane being attached\nto \"mother\" B-50--B-50 taxis,taking off and in flight--\"mother\"plane\ndrops the X-2 and it glides to ground (not using power at all,Just\ngliding)--landing, coming to halt on skis\nINFORMATION: (This\nsuccessor to the K-1A--It was built to probe the thermal barrier,as a\nflying research laboratory--to investigate probéems beyond the speed\nsound ans to surpass speed of 1650 MPH-- \"mother\"plane carries vehicle\nto specified altitude where it begins its flight on its own power--th\nconserves fuel and power for longer flight--skis replace wheeis\nto\nfu:\nther reduce weight to aid speed--built by Bell Aircraft in conjuntion\nSEE OVER\nPRINTED IN U.S.A.\nFORM 2530-8M-12/68\nOVER"
}