Burning Rates of Solid Propellants
- 1 January 1960
- journal article
- research article
- Published by AIP Publishing in The Journal of Chemical Physics
- Vol. 32 (1), 89-93
- https://doi.org/10.1063/1.1700952
Abstract
The burning mechanism of a solid propellant is described in terms of a pyrolysis law, a premixed laminar flame, and nothing more. A quantitatively accurate burning rate formula is derived from the theory. The predicted burning rate pressure dependence agrees with the experimental results for ammonium perchlorate propellants.This publication has 2 references indexed in Scilit:
- H Theorems for One-Dimensional Combustion of a GasThe Journal of Chemical Physics, 1959
- Direct Determination of Burning Rates of Propellant PowdersAnalytical Chemistry, 1947