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APOLLO ABLATOR THERMAL PERFORMANCE AT SUPERORBITAL ENTRY VELOCITIES

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BookPublisher: Nasa, Washington, D.C. 1970Description: 26.DDC classification: NASA | TN D-5969 -

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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 TN D-5969 - (Browse shelf)	Not for loan		TR9427

Total holds: 0

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Previous	NASA TN D-5966 - NASA MINITRACK INTERFEROMETER REFRACTION CORRECTIONS	NASA TN D-5967 - STRESS EFFECTS OF HIGH NOISE LEVELS ON LOWER BODY NEGATIVE PRESSURE EXPERIMENTS	NASA TN D-5968 - INVESTIGATION OF THE INITIAL CENTURY SERIES RINGSAIL PARACHUTE	NASA TN D-5969 - APOLLO ABLATOR THERMAL PERFORMANCE AT SUPERORBITAL ENTRY VELOCITIES	NASA TN D-5971 LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A TWIN-TURBOFAN SUBSONIC TRANSPORT WITH NACELLES MOUNTED UNDER THE WINGS	NASA TN D-5972 INVESTIGATION OF AN OPTIMUM DETECTION SCHEME FOR A STAR-FIELD MAPPING SYSTEM	NASA TN D-5973 EFFECT OF STRAIN-GAGE ATTACHMENT BY SPOTWELDING AND BOUNDING ON FATIGUE BEHAVIOR OF TI-6A1-4V, RENE 41, AND INCONEL X	Next

Bound With Nasa Tn D-5960-69

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