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FIXED-BASE VISUAL SIMULATION OF OBSTACLE A VOIDANCE DURING TERMINAL DESCENT OF ADVANCED APOLLO SPACECRAFT WITH ALL-FLEXIABLE PARAWING.

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BookPublisher: NASA, WASHINGTON, D.C. 1970Description: ,49.DDC classification: NASA | TN D-5940

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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-5940 (Browse shelf)	Not for loan		101212

Total holds: 0

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Previous	NASA TN D-5831 APPLICATION OF ANALYSIS AND MODELS TO STRUCTURAL DYNAMIC PROBELMS RELATED TO THE APOLLO-SATURN V LAUNCH VEHICLE.	NASA TN D-5881 DEVELOPMENT AND EVALUATION OF A HIGH-EFFICIENCY POWER INVERTER	NASA TN D-5920 CONTROL OF ELECTRONIC CIRCUIT DESIGNS FOR SPACE VECHICLES.	NASA TN D-5940 FIXED-BASE VISUAL SIMULATION OF OBSTACLE A VOIDANCE DURING TERMINAL DESCENT OF ADVANCED APOLLO SPACECRAFT WITH ALL-FLEXIABLE PARAWING.	NASA TN D-5950 TRAJECTORY OBSERVATIONS FOR SOME SPIRALING-ELECTRON BEAM SYSTEMS	NASA TN D-5970 AN INTEGRAL ANALYSIS OF HEAT TRANSFER DOWNSTREAM OF A REARWARD-FACING STEP WITH SMALL COOLANT INJECTION	NASA TN D-5990 FRICTION AND CONTACT RESISTANCE FOR GALLIUM-LUBRICATED LOW-SPEED COPPER SLIPRINGS IN VACUUM.	Next

Bound with NASA TN D-5941-5949.

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