Question: A rocket has Pc = 2 0 0 atm, Tc = 3 7 5 0 K , R = 5 0 0 J / kg

A rocket has Pc =200 atm, Tc =3750 K, R =500 J/kg-k, =1.4, Pa =10,000 N/m2
, Ae =1.6 m2
, A*=0.05 m2
. Assume the nozzle is isentropic. Find the thrust and the Isp for this rocket.

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