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WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.40 TO 1.20 OF THE STATIC AERODYNAMIC AND CONTROL CHARACTERISTICS OF A MODEL OF A NONLIFTING REENTRY CAPSULE IN COMBINATION WITH A ROCKET BOOSTER

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BookPublisher: Nasa, Washington, D.C. 1960Description: 63.DDC classification: NASA | TM X-317

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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-317 (Browse shelf)	Not for loan		TR16066

Total holds: 0

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Previous	NASA TM X-31 - APPROACH AND LANDING INVESTIGATION AT LIFT-DRAG RATIOS OF 2 TO 4 UTILIZING A STRAIGHT-WING FIGHTER AIRPLANE	NASA TM X-313 STRUCTURES FOR REENTRY HEATING	NASA TM X-314 EXPERIMENTAL STUDY OF A HOT STRUCTURE FOR A REENTRY VEHICLE	NASA TM X-317 WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.40 TO 1.20 OF THE STATIC AERODYNAMIC AND CONTROL CHARACTERISTICS OF A MODEL OF A NONLIFTING REENTRY CAPSULE IN COMBINATION WITH A ROCKET BOOSTER	NASA TM X-33 - ELEVATED-TEMPERATURE TESTS UNDER STATIC AND AERODYNAMIC CONDITIONS ON HONEYCOMBCORE SANDWICH PANELS	NASA TM X-332 AERODYNAMIC CHARACTERISTICS AT MACH NUMBER 2.05 OF A SERIES OF HIGHLY SWEPT ARROW WINGS EMPLOYING VARIOUS DEGREES OF TWIST AND CAMBER	NASA TM X-336 PRESSURE DISTRIBUTION ON TWO MODELS OF A PROJECT MERCURY CAPSULE FOR A MACH NUMBER RANGE OF 1.60 TO 6.01 AND AN ANGLE-OF-ATTACK RANGE OF 0 DEGREE TO 180 DEGREE	Next

Bound With Nasa Tm X-300-14,332-45 Lack No.301-04,306-12,315-16,318-31,333,335,337,339-43

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