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EXPERIMENTAL INVESTIGATIO OF CLOSE-RANGE ROCKET-EXHAUST IMPINGEMENT ON SURAFCES IN A VACUUM

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BookPublisher: Nasa, Washington, D.C. 1970Description: 29.DDC classification: NASA | TN D-5895 -

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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-5895 - (Browse shelf)	Not for loan		TR8804

Total holds: 0

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Previous	NASA TN D-5890 EVALUATION OF THE EFFECT OF A YAW-RATE DAMPER ON THE FLYING QUALITIES OF A LIGHT TWIN-ENGINE AIRPLANE	NASA TN D-5893 - MODEL WIND-TUNNEL AND FLIGHT INVESTIGATION OF A PARAWING-LIFTING-BODY LANDING SYSTEM	NASA TN D-5894 - THE SIMULATION OF IONOSPERIC CONDITONS FOR SPACE VEHICLES	NASA TN D-5895 - EXPERIMENTAL INVESTIGATIO OF CLOSE-RANGE ROCKET-EXHAUST IMPINGEMENT ON SURAFCES IN A VACUUM	NASA TN D-5896 - METHOD FOR DETERMINATION OF THE ACCURACY OF CLOSED DISTANT STATIONARY ORBITS DETERMINED FROM RANGE RANGE RATE	NASA TN D-5897 - EXPERIMENTAL DETERMINATION OF APPARENT MASS AND MOMENT OF INERTIA OF A LARGE DISK SUSPENDED AS A PENDULUM AT DIFFERENT AIR DENSITIES	NASA TN D-5898 - AERODYNAMIC INTERFERENCE EFFECTS ON HALF-CONE BODIES WITH THIN WINGS AT MACH 10.03	Next

Bound With Nasa Tn D-5891-99

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