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ANALYTICAL MODEL FOR DETERMINING SPACECRAFT IMPACT VELOCITY AND ORIENTATION RELATIVE TO AN IMPACT SURFACE

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BookPublisher: Nasa, Washington, D.C. 1971Description: 21.DDC classification: NASA | TN D-6325

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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-6325 (Browse shelf)	Not for loan		TR15159

Total holds: 0

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Previous	NASA TN D-6322 BUCKLING LOAD OF THIN CIRCULAR CYLINDRICAL SHELLS FORMED BY PLASTIC EXPANSION	NASA TN D-6323 LARGE-SCALE WIND-TUNNEL INVESTIGATION OF A DUCTED-FAN-DEFLECTED-SLIPSTREAM MODEL WITH AN AUXILIARY WING	NASA TN D-6324 A STUDY OF LOW-VELOCITY IMPACTS INTO THIN-SHEET ALUMINUM AND NYLON CLOTH	NASA TN D-6325 ANALYTICAL MODEL FOR DETERMINING SPACECRAFT IMPACT VELOCITY AND ORIENTATION RELATIVE TO AN IMPACT SURFACE	NASA TN D-6326 FINITE-ELEMENT MODELING STUDIES IN THE NORMAL-MODE METHOD AND NORMAL-MODE SYNTHESIS	NASA TN D-6328 LONGITUDINAL INSTABILITY LIMITS WITH A VARIABLE-LENGTH HYDROGEN-OXYGEN COMBUSTOR	NASA TN D-6331 EXPERIMENTAL EVALUATION OF A PURGED SUBSTRATE MULTILAYER INSULATION SYSTEM FOR LIQUID HYDROGEN TANKAGE.	Next

Bound With Nasa Tn D-6321-24,6326-29 Lack No.6327

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