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ION-THRUSTER PROPELLANT UTILIZATION

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BookSeries: NASA Technical Note. Publisher: NASA, Washington, D.C. 1971Description: 56p.Subject(s): Aerodynamics

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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-6591	Not for loan		TR9345

Total holds: 0

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Previous	NASA Technical Note [NASA TN D-3448]: Energy transport by thermal field emission	NASA Technical Note [NASA TN D-3449]: Effects of subcooling and gravity level on boiling in the discrete bubble region	NASA Technical Note [NASA TN D-3450]: A review of some existing literature concerning discontinuous state variables in the calculus of variations	ION-THRUSTER PROPELLANT UTILIZATION	MIXING OF SUPERSONIC JETS INCLUDING THE EFFECTS OF TRANSVERSE PRESSURE GRADIENT USING DIFFERENCE METHODS	FIELD EVAPORATION ION SOURCE WITH POSSIBLE APPLICATION TO ELECTROSTATIC PROPULSION	HEAT TRANSFER AND BOUNDARY LAYER IN CONICAL NOZZLES	Next

Technical Reports D-6590-96
Bound Vol. No.101254; contents: TR9345-53

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