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PERFORMANCE OF A SMALL GAS GENERATOR USING LIQUID HYDROGEN AND LIQUID OXIGEN

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BookPublisher: Nasa, Washington, D.C. 1961Description: 33.DDC classification: NASA | TM X-417

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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-417 (Browse shelf)	Not for loan		TR1652

Total holds: 0

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Previous	NASA TM X-344 BASIC PRESSURE MEASUREMENTS ON A 0.0667-SCALE MODEL OF THE NORTH AMERICAN X-15 RESEARCH AIRPLANE AT TRANSONIC SPEEDS	NASA TM X-36 - FLIGHT INVESTIGATION OF THE EFFECT OF DISTRIBUTION ROUGHNESS ON SKIN DRAG OF A FULL-SCALE AIRPLANE	NASA TM X-39 - DYNAMIC LONGITUDINAL AND DIRECTIONAL STABILITY DERIVATIVES FOR A 45[DEGREE] SWEPTBACK-WING AIRPLANE MODEL AT TRANSONIC SPEEDS	NASA TM X-417 PERFORMANCE OF A SMALL GAS GENERATOR USING LIQUID HYDROGEN AND LIQUID OXIGEN	NASA TM X-423 STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS AT TRANSONIC SPEEDS OF A LENTICULAR-SHAPED REENTRY VEHICLE	NASA TM X-425 FREE-FLIGHT INVESTIGATION AT SUPERSONIC SPEEDS OF THE STABILITY AND DRAG OF A 79 DEGREE C CLIPPED DELTA BOOST-GLIDE CONFIGURATION INCLUDING AN ANALOG STUDY OF COUPLED MOTIONS DURING THE FLIGHT	NASA TM X-427 AN INVESTIGATION OF THE INFLUENCE OF BODY SIZE AND INDENTATION ASYMMETRY ON THE EFFECTIVENESS OF BODY INDETATION IN COMBINATION WITH A CAMBERED WING	Next

Bound With Nasa Tm X-416,423-79 Lack No.418-22,24,26,28-29,32,34-36,38,42-47,50-58,60-66,69-78

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