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CONTROLLABILITY OF THE X-15 RESEARCH AIRPLANE WITH INTERIM ENGINES DURING HIGH-ALTITUDE FLIGHTS

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BookPublisher: Nasa, Washington, D.C. 1961Description: 21.DDC classification: NASA | TM X-514

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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-514 (Browse shelf)	Not for loan		TR14305

Total holds: 0

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Previous	NASA TM X-468 SKIN AND STRUCTURAL TEMPERATURES MEASURED ON THE X-15 AIRPLANE DURING A FLIGHT TO A MACH NUMBER OF 3.3	NASA TM X-479 A PHOTOGRAPHIC STUDY OF LIQUID HYDROGEN UNDER SIMULATED ZERO GRAVITY CONDITIONS	NASA TM X-508 MEASUREMENTS OF THERMAL RADIATION OF AIR FROM THE STAGNATION REGION OF BLUNT BODIES TRAVELING AT VELOCITIES UP TO 31,000 FEET PER SECOND	NASA TM X-514 CONTROLLABILITY OF THE X-15 RESEARCH AIRPLANE WITH INTERIM ENGINES DURING HIGH-ALTITUDE FLIGHTS	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	Next

Bound With Nasa Tm X-507-508,518-81 Lack No.509-13,515-17,519-21,523-29,531-39,541-46,548-65,567-68,572-80

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