Effects of the Burning Rate Index on the Pressure Time Profile of Progressive Burning Tubular Rocket Propellant Configurations – Łukasiewicz-IPO

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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