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Rocket basics fuel in e Thrust Oxidizer in A Throat Thrust eret Aelpe-p) F=ny Specific impulse SD≡ F mg Isp=K where k depends on y and the engine pressure ratioRocket Basics Thrust Specific impulse where K depends on J and the engine pressure ratio ( ) f   p ep eA eVe F m M cT Isp K mg Isp F {  me Ve Pe Ae fp Fuel in Oxidizer in Thrust pc Throat
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