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Aerodynamic characteristics from Mach 0.22 to 4.65 of a two-stage rocket vehicle having an unusual nose shape

By: Suttles, John T.

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BookSeries: National Aeronautics and Space Administration [NASA]. Publisher: Washington, D.C. National Aeronautics and Space Administration [NASA] 1964DDC classification: NASA | TN D-2163

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)	NASA TN D-2163 (Browse shelf)	Not for loan		TR013472

Total holds: 0

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Previous	NASA TN D-2161 An instrument for electronic differentiation of current voltage characters [NASA TN D-2161--TN D-2170]	NASA TN D-2162 Examination of onboard training for extended space flights [NASA TN D-2162]	NASA TN D-2163 AERODYNAMIC CHRACTERISTICS FROM MACH 0.22 TO 4.65 OF A TWO-STAGE ROCKET VEHICLE HAVING AN UNUSAL NOSE SHAPE.	NASA TN D-2163 Aerodynamic characteristics from Mach 0.22 to 4.65 of a two-stage rocket vehicle having an unusual nose shape	NASA TN D-2164 ELECTROMAGNETIC ACCELERATION OF QA VARIABLE-MASS PLASMA	NASA TN D-2164 Electromagnetic acceleration of a variable-mass plasma	NASA TN D-2165 Comparison of measurements of internal temperatures in ablation material by various thermocouple configurations	Next

Bound with NASA TN D-2162-2170

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