2010•Journal of Solid Rocket TechnologyRequires access

Theoretical performance analysis of Mg/CO_2 powdered rocket engine

Guoqiang He

Abstract

The theoretical performance of the powdered rocket engine is calculated theoretically in considering the specific impulse and the impact of factors.Compared with the traditional propulsion system,the powdered rocket engine has better specific impulse.In the calculation research of the performance of Mg and CO2,the rules of burning pressure,starting temperature and oxidizer-to-fuel ratio(by mass) were obtained.

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Key concepts: Specific impulse, Rocket engine, Impulse (physics), Rocket (weapon), Rocket propellant, Aerospace engineering, Propulsion, Materials science