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MINIMUM PROPELLANT CONSUMPTION ROUND-TRIP TRAJECTORIES TO MARS FOR CONSTANT-THRUST, CONSTANT-SPECIFIC-IMPULSE VEHICLES WITH OPTIMUM COASTING PERIODS

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BookPublisher: NASA, Washington, D.C. 1966Description: 32.Subject(s): Aerodynamics

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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)		Not for loan		TR7415

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Previous	Further developments on the required number of randomly spaced communication and navigation satellites[NASA TN D -1020]	NASA TM [X-72]	MECHANICAL PROPERTIES AND RECRYSTALLIZATION BEHAVIOR OF ELECTRON -BEAM-MELTED TUNGSTEN COMPARED WITH ARC-MELTED TUNGSTEN	MINIMUM PROPELLANT CONSUMPTION ROUND-TRIP TRAJECTORIES TO MARS FOR CONSTANT-THRUST, CONSTANT-SPECIFIC-IMPULSE VEHICLES WITH OPTIMUM COASTING PERIODS	THERMAL RADIATION ABSORPTANCE AND VACUUM OUTGASSING CHARACTERISTICS OF SEVERAL METALLIC AND COATED SURFACES	FRICTION, WEAR, AND ADHESION CHARACTERISTICS OF TITANIUM-ALUMINUM ALLOYS IN VACUUM	NASA TM [X-786]	Next

Technical Reports D-3231-40
Bound Vol. No.65618; contents: TR7414-7422

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