System for nondissipative control of mass-flow from solid propellant gas generator is proposed; primary hypothesis of system (that propellant gas efflux can be modulated through intercession of counter-flow heat exchanger that improves heat flux from gas to solid) is studied analytically and experimentally; significant changes in burning rate can be made to occur with rams of practical design and with acceptable values of pertinent parameters; system studies incorporating models of phenomena have indicated that constant-mass flow, despite environmental temperature, and demand flow gas generators are feasible.
Control of solid propellant combustion
J Spacecraft Rockets
Journal of Spacecraft and Rockets ; 3 , n 8
1966
6 pages
Aufsatz (Zeitschrift)
Englisch
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Control of solid propellant combustion.
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