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Effect of oxidizer particle size on solid- propellant combustion stability [NASA TN D-2736]

By: Morrell, G.

Contributor(s): Pinns, M. L.

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BookSeries: National Aeronautics and Sapce Administration (NASA). Publisher: Nasa Washington, D. C. 1965Description: 13p.Subject(s): combustion stability

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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-2736 (Browse shelf)	Not for loan		TR64276 (e)

Total holds: 0

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Previous	NASA TN D-2733 Laboratory experiments on the performance of silicon solar cells at high solar intensities and temperatures [NASA TN D-2733]	NASA TN D-2734 Solubility of iron, nickel, and cobalt in liquid potassium and effect of oxygen gettering agents on iron solubility [NASA TN D-2734]	NASA TN D-2735 Techniques for improving the opening of the main diaphragm in a large combustion driver [NASA TR D-2735]	NASA TN D-2736 Effect of oxidizer particle size on solid- propellant combustion stability [NASA TN D-2736]	NASA TN D-2737 Experimentally determined pendulum analogy of liquid sloshing in spherical and oblate- spheroidal tanks [NASA TN D-2737]	NASA TN D-2738 Rates of hydrogen-graphite reaction between 1550 deg and 2260 deg c [NASA TN D-2738]	NASA TN D-2739 Comparison of direct and indirect ascent modes for the 1966-1967 mars opportunity with an atlas-centaur launch vehicle [NASA TN D- 2739]	Next

NASA technical report

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