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SOME OPERATIONAL ASPECTS OF USING A HIGH-PERFORMANCE AIRPLANE AS A FIRST-STAGE BOOSTER FOR AIR-LAUNCHING SOLID-FUEL SOUNDING ROCKETS

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BookPublisher: Nasa, Washington, D.C. 1963Description: 22.DDC classification: NASA | TN D-1279

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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-1279 (Browse shelf)	Not for loan		TR14809

Total holds: 0

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Previous	NASA TN D-1276 GROUND FACILITY REQUIREMENTS FOR SUBCOOLING LIQUID HYDROGEN	NASA TN D-1277 STUDIES IN FAR-FIELD ACOUSTIC PROPAGATION	NASA TN D-1278 REVIEW OF THE X-15 PROGRAM	NASA TN D-1279 SOME OPERATIONAL ASPECTS OF USING A HIGH-PERFORMANCE AIRPLANE AS A FIRST-STAGE BOOSTER FOR AIR-LAUNCHING SOLID-FUEL SOUNDING ROCKETS	NASA TN D-128 FLAME STABILITY EFFECT OF GASES EJECTED INTO A STREAM FROM A BLUFF-BODY FLAMEHOLDER	NASA TN D-1280 APPROXIMATE ANALYSIS OF G LOADS AND HEATING DURING ATMOSPHERIC ENTRIES AND PASSES WITH CONSTANT AERODYNAMIC COEFFICIENTS	NASA TN D-1282 - SMOOTH AND SHARP-NOTCH PROPERTY VARIATIONS FOR SEVERAL HEATS OF TI-6AL-4V SHEET AT ROOM AND CRYOGENIC TEMPERATURES	Next

Bound With Nasa Tn D-1271-78,1280

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