Composite solid propellant - Open Access .click

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Subcritical Crack Growth in a Composite Solid Propellant

Journal of Reinforced Plastics and Composites, 1999
Uniaxial tension tests using a strain rate of 0.04 in./in./min. are performed on rectangular smooth and single edge-notched specimens of varying thicknesses for a composite solid propellant. Stress-strain, crack growth, crack growth rate and crack growth resistance data are provided.
D. T. Baron, T. C. Miller, C. T. Liu
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Theoretical detonation characteristics of solid composite propellants.

AIAA Journal, 1965
1 Bulewicz, E. M. and Padley, P. J., "A. cyclotron resonance study of ionization in low-pressure flames," Ninth International Symposium on Combustion (Academic Press, Inc., New York, 1963). 2 Azatian, V. V., Panilov, V. N., and Nalbandyan, A. B., "EPR detection of N atoms in CO-O2 flame in the presence of molecular H2," Kinetika i Kataliz 2 (March ...
W. H. ANDERSEN, O. R. IRWIN, P. K. SALZMAN +2 more
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Continuous measurement of the burning rate of a composite solid propellant.

AIAA Journal, 1967
A method for continuous, high-resolution measurement of the burning rate of a solid propellant has been devised and used successfully in preliminary tests. The method consists of using a solid-propellant strand as the dielectric material of a capacitor forming a part of a resonant L-C circuit oscillating at a center frequency of 10.7 MHz.
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Recent advances in catalytic combustion of AP-based composite solid propellants

Defence Technology, 2021
Dr Narendra Yadav
exaly

Thermal decomposition and combustion behavior of solid propellant containing Si-based composites

Combustion and Flame, 2022
Pei-Jin Liu, Qi-Long Yan
exaly

Mechanistic studies on composite-solid propellants