- #1
Jedi_Sawyer
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Does anybody know how or where I can find a way to figure the Exhaust Temperature of a Rocket. I am considering a problem where I assigned 1.4 atmospheres to the Inlet gas pressure at 300 degrees C.
That it exited into 1 Atmosphere at exit velocity of 325 M per second.
That it exited into 1 Atmosphere at exit velocity of 325 M per second.