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WIND-TUNNEL INVESTIGATION OF STATIC AERODYNAMIC CHARACTERISTICS OF A 1/9-SCALE MODEL OF A POSSIBLE REENTRY CAPSULE AT MACH NUMBERS FROM 2.29 TO 4.65

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BookPublisher: Nasa, Washington, D.C. 1959Description: 19.DDC classification: NASA | TM X-233 -

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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-233 - (Browse shelf)	Not for loan Untraceable		TR8826

Total holds: 0

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Previous	NASA TM X-227 - LOW-SUBSONIC-SPEED STATIC LONGITUDINAL STABILITY AND CONTROL CHARACTERISTICS OF A WINGED REENTRY-VEHICLE CONFIGURATION HAVING WINGTIP PANELS THAT FOLD UP FOR HIGH-DRAG REENTRY	NASA TM X-23 - CHARACTERISTICS OF FIVE EJECTOR CONFIGURATIONS AT FREE-STREAM MACH NUMBERS FROM 0 TO 2.0	NASA TM X-232 - HIGH-ALTITUDE PERFORMANCE OF A 64-FOOT-DIAMETER RING SAIL PARACHUTE	NASA TM X-233 - WIND-TUNNEL INVESTIGATION OF STATIC AERODYNAMIC CHARACTERISTICS OF A 1/9-SCALE MODEL OF A POSSIBLE REENTRY CAPSULE AT MACH NUMBERS FROM 2.29 TO 4.65	NASA TM X-235 - EXPERIMENTAL INVESTIGATION AND CORRELATION OF THE HEAT REDUCTION TO NONPOROUS SURFACES BEHIND A POROUS LEADING EDGE THROUGH WHICH COOLANT IS EJECTED	NASA TM X-24 - AERODYNAMIC CHARACTERISTICS OF A 0.0667-SCALE MODEL OF THE NORTH AMERICAN X-15 RESEARCH AIRPLANE AT TRANSONIC SPEEDS	NASA TM X-240 - HYPERSONIC LONGITUDINAL TRIM, STABILITY, AND CONTROL CHARACTERISTICS OF A DELTA-WING CONFIGURATION AT HIGH ANGLES OF ATTACK	Next

Bound With Nasa Tm X-205-49

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