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PLASMA ACCELERATION BY USE OF GUIDED MICROWAVES [NASA TN D-46]

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BookPublisher: Washington, D.C. National Aeronautics and Space Administration 1959Description: 46p.

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Item type	Current location	Collection	Call number	Vol info	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		NASA TN D 41-50	Not for loan		TR010894

Total holds: 0

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Previous	AN EVALUATION OF LINEARIZED VORTEX THEORY AS APPLIED TO SINGLE AND MULTIPLE ROTORS HOVERING IN AND OUT OF GROUND EFFECT [NASA TN D-43]	FORCE-TEST INVESTIGATION OF THE STABILITY AND CONTROL CHARACTERISTICS OF A 1/8-SCALE MODEL OF A TILT-WING VERTICAL-TAKE-OFF-AND-LANDING AIRPLANE [NASA TN D-44]	FLIGHT INVESTIGATION OF STABILITY AND CONTROL CHARACTERISTICS OF A 1/8-SCALE MODEL OF A TILT-WING VERTICAL-TAKE-OFF-AND-LANDING AIRPLANE [NASA TN D-45]	PLASMA ACCELERATION BY USE OF GUIDED MICROWAVES [NASA TN D-46]	DYNAMIC ANALYSIS OF A SIMPLE REENTRY MANEUVER FOR A LIFTING SATELLITE.[NASA TN D-47]	SOME ASPECTS OF AIR-HELIUM SIMULATION AND HYPERSONIC APPROXIMATIONS [NASA TN D-49]	WIND-TUNNEL INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF A MODEL REPRESENTATIVES OF A SUPERSONIC FIGHTER-CLASS AIRPLANE WITH AN EXTERNAL-FLOW JET-AUGMENTED FLAP IN LOW-SPEED FLIGHT [NASA TN D-50]	Next

Bounds vol. contains Nasa TN D 41-50

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