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Experimental effects of propellant-introduction mode on electron-bombardment ion rocket performance [NASA TN D-2587]

By: Reader, Paul D.

Contributor(s): Reader, Paul D.

Material type: materialTypeLabel

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BookSeries: National Aeronautics and Space Administration (NASA). Publisher: Washington, D.C. Nasa, Washington, D.C. 1965Description: 24p.Subject(s): rocket performance

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NASA technical report

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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)	NASA TN D-2587 (Browse shelf)	Not for loan		TR15756

Total holds: 0

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Previous	NASA TN D-2584 Some effects of uncertainties in atmosphere structure and chemical composition on entry into mars [NASA TN D-2584]	NASA TN D-2585 An analysis of the problem of tank pressurization during outflow [NASA TN D-2585]	NASA TN D-2586 Model investigation of technique for conducting full-scall landing-impact tests at simulated lunar gravity [NASA TN D-2586]	NASA TN D-2587 Experimental effects of propellant-introduction mode on electron-bombardment ion rocket performance [NASA TN D-2587]	NASA TN D-2588 Quadrature formulas for the a and operators of radiative transfer [NASA TN D- 2588]	NASA TN D-2589 Application of the double spherical harmonics method to the one-dimensional radiation-transfer equation [NASA TN D-2589]	NASA TN D-2590 Determination of loads on a flexible launch vehicle during ascent through winds [NASA TN D-2590]	Next

NASA technical report

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