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- W776013167 abstract "Reported study of composite-propellant burning summarizes recent advances in understanding behavior of propellant formulations based on ammonium perchlorate (AOP), binder, and aluminum in various proportions and particle size distributions. Approach presented incorporates adapted version of earlier model for monopropellant AP. Objective is to predict burning-rate characteristics of composite propellants at high pressure." @default.
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- W776013167 date "1983-03-01" @default.
- W776013167 modified "2023-09-22" @default.
- W776013167 title "Equations for Composite-Propellant Burning" @default.
- W776013167 hasPublicationYear "1983" @default.
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