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INVESTIGATION OF LOW-SUBSONIC STABILITY AND CONTROL CHARACTERISTICS OF A 0.34-SCALE FREE-FLYING MODEL OF A MODIFIED HALF-CONE REENTRY VEHICLE

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BookPublisher: Nasa, Washington, D.C. 1962Description: 41.DDC classification: NASA | TMX-665 -

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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 TMX-665 - (Browse shelf)	Not for loan		TR8993

Total holds: 0

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Previous	NASA TM X-953 NATIONAL ALTITUDE ROCKET TEST FACILITIES.	NASA TMX-639 - LANDING LOADS AND DYNAMICS OF THE X-15 AIRPLANE	NASA TMX-652 - EXPERIMENTAL INVASTIGATION OF A DISK-SHAPED REENTRY CONFIGURATION AT TRANSONIC AND LOW SUPERSONIC SPEEDS	NASA TMX-665 - INVESTIGATION OF LOW-SUBSONIC STABILITY AND CONTROL CHARACTERISTICS OF A 0.34-SCALE FREE-FLYING MODEL OF A MODIFIED HALF-CONE REENTRY VEHICLE	NASA TMX-680 - WIND-TUNNEL INVESTIGATION OF THE AERODYNAMIC AND STRUCTURAL-DEFLECTION CHARACTERISTICS OF AN INFLATABLE AIRPLANE	NASA TN 32-872 THERMOELECTRIC POWER IN NIOBIUM-ZIRCONIUM ALLOYS	NASA TN 32-873 FAR-INFRARED REFLECTANCE OF SPACECRAFT COATINGS	Next

Bound With Nasa Tmx-606,39,52,65,80

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