Effects of the Burning Rate Index on the Pressure Time Profile of Progressive Burning Tubular Rocket Propellant Configurations

Posted on 04 kwietnia, 2021 by Michał Gańko in CEJEM, Vol 12 Nr 2

Effects of the Burning Rate Index on the Pressure Time Profile of Progressive Burning Tubular Rocket Propellant Configurations

Himanshu SHEKHAR
Słowa Kluczowe: rocket propellant, burning rate, pressure time, progressive burning, tubular configuration
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