Combustion of a propellant and its extinction upon rapid depressurization: A comparison of theory and experiment

Marshakov, V. N.; Novozhilov, B. V.

doi:10.1134/s1990793111020369

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2023

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Cited by 8 publications

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“…Kuo and Coates [1] and Gusachenko and Zarko [2] reviewed the previous works. Recently, the extinction problem of solid propellant during depressurization was investigated by Marshakov et al [3,4] using the phenomenological theory. However, when the base bleed projectile is propelled out of the muzzle, the AP/HTPB propellant in the base bleed unit suffers a much more severe transient depressurization than that in the rocket motor, which may destabilize the propellant combustion and bring unfavourable effect to the firing precision.…”

Section: Introductionmentioning

confidence: 99%