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EFFECT OF NOSE-MOUNTED CONTROL-SYSTEM JETS IN ROLL-CONTROL POSITIONS ON THE AERODYNAMICS OF A SPACE VEHICLE

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BookPublisher: Nasa, Washington, D.C. 1966Description: 26.DDC classification: NASA | TN D-3282 -

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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-3282 - (Browse shelf)	Not for loan		TR10031

Total holds: 0

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Previous	NASA TN D-3279 A PHOTOVOLTAIC SOLAR SENSOR FOR USE IN SPACECRAFT ORIENTATION CONTROL SYSTEMS	NASA TN D-328 PHOTOGRAPHIC EVIDENCE OF STREAMWISE ARRAYS OF VORTICES IN BOUNDARY- LAYER FLOW.	NASA TN D-3280 ANALYTICAL INVESTIGATION OF THE MOTION OF A CLAMSHELL-TYPE HEAT SHIELD ON DEVELOPMENT FROM A PARENT VEHICLE IN THE ATMOSPHERE	NASA TN D-3282 - EFFECT OF NOSE-MOUNTED CONTROL-SYSTEM JETS IN ROLL-CONTROL POSITIONS ON THE AERODYNAMICS OF A SPACE VEHICLE	NASA TN D-3283 - EMPIRICAL METHOD FOR DETERMINING STATIC DISTRIBUTED AERODYNAMIC LOADS ON AXISYMMETRIC MULTISTAGE LAUNCH VEHICLES	NASA TN D-3284 - EFFECT OF NACELLE ORIENTATION OF THE AERODYNAMIC CHARACTERISTICS OF AN ARROW WING-BOLY CONFIGURATION AT MACH NUMBER 2.03	NASA TN D-3285 - FLOW FIELD SURVEY AND DECELERATOR DRAG CHARACTERISTICS IN THE WAKE OF A MODEL OF THE X-15 AIRPLANE AT MACH 2.0 AND 4.65	Next

Bound With Nasa Tn D-3281-90

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