Question: A rocket has P c = 1 5 2 atm, T c = 3 6 0 0 K , R = 5 0 0 J

A rocket has Pc=152atm,Tc=3600K,R=500Jkg-K,=1.4,Pa=10kPa,Ae=1.308m2,
A*=0.122m2. Assume that the nozzle is isentropic. For this rocket, find the thrust, Isp, the effective
exhaust velocity, and the characteristic velocity.
A rocket has P c = 1 5 2 atm, T c = 3 6 0 0 K , R

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