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A PRELIMINARY STUDY OF SOME ABORT TRAJECTORIES INITIATED DURING LAUNCH OF A LUNAR MISSION VEHICLE

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BookPublisher: Nasa, Washington, D.C. 1961Description: 27.DDC classification: NASA | TM X-530

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TM X-530 (Browse shelf)	Not for loan		TR14309

Total holds: 0

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Previous	NASA TM X-518 LANDING-GEAR BEHAVIOR DURING TOUCHDOWN AND RUNOUT FOR 17 LANDINGS OF THE X-15 RESEARCH AIRPLANE	NASA TM X-519 EFFECT OF VERTICLE-TAIL MODIFICATIONS ON THE STATIC STABILITY CHARACTERISTICS AT A MACH NUMBER OF 2.2 OF A SUPERSONIC VTOL AIRPLANE MODEL HAVING A BROAD FUSELAGE AND SMALL DELTA WINGS	NASA TM X-522 HEAT-TRANSFER AND PRESSURE MEASUREMENTS OF A 1/7-SCALE MODEL OF A MERCURY CAPSULE AT ANGLES OF ATTACK FROM 0 DEGREE TO +- 20 DEGREE AT MACH NUMBERS OF 3.50 AND 4.44	NASA TM X-530 A PRELIMINARY STUDY OF SOME ABORT TRAJECTORIES INITIATED DURING LAUNCH OF A LUNAR MISSION VEHICLE	NASA TM X-540 AN INVESTIGATION OF MODIFIED CLUSTERED JET-EXIT ARRANGEMENTS AT SUPERSONIC SPEEDS	NASA TM X-547 WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.30 TO OF THE STATIC AERODYNAMIC CHARACTERISTICS OF MODIFIED MERCURY ESCAPE AND EXIT CAPSULE CONFIGURATIONS	NASA TM X-566 SUBSONIC AERODYNAMIC CHARACTERISTICS OF DISK RE-ENTRY CONFIGURATIONS WITH ELLIPTIC CROSS SECTIONS AND THICKNESS-DIAMETER RATIOS OF 0.225 AND 0.325	Next

Bound With Nasa Tm X-507-22,540-81,Lack No.509-13,515-17,519-21,523-29,531-39,541-46,548-65,567-68,572-80

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