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SIMULATOR STUDY OF PILOT CONTROL OF REMOTE ORBITAL DOCKING OF LARGE ATTITUDE-STABILIZED COMPONENTS

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BookPublisher: Nasa, Washington, D.C. 1967Description: 21.DDC classification: NASA | TN D-4263 -

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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-4263 - (Browse shelf)	Not for loan		TR9188

Total holds: 0

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Previous	NASA TN D-4259 BALLISTIC LIMIT OF ALUMIUM PLATES DETERMINED BY AN EXPLODING FOIL GUN TECHNIQUE	NASA TN D-4260 THREE BALLISTIC CAMERA DATA REDUCTION METHODS APPLICABLE TO REENTRY EXPERIMENTS	NASA TN D-4262 - WIND-TUNNEL INVESTIGATION OF A DEFLECTED-SLIPSTREAM CRUISE-FAN V/STOL AIRCRAFT WING	NASA TN D-4263 - SIMULATOR STUDY OF PILOT CONTROL OF REMOTE ORBITAL DOCKING OF LARGE ATTITUDE-STABILIZED COMPONENTS	NASA TN D-4264 - SOME METEOROLOGICAL OBSERVATIONS OF THE SOUTHERN HEMISPHERE STRATOSPHERE AND MESOSPHERE	NASA TN D-4265 - NONLINEAR FLUTTER OF A CIRCULAR CYLINDRICAL SHELL IN SUPERSONIC FLOW	NASA TN D-4266 - FLIGHT TEST OF A 15-FOOT-DIAMETER (4.6-METER) 120[DEGREE] CONICAL SPACECRAFT SIMULATING PARACHUTE DEPLOYMENT IN A MARS ATMOSPHERE	Next

Bound With Nasa Tn D-4261-70

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