- May 23, 2020
- Reaction score
Hello! I am designing a cold gas thruster for a project that will use either N2 or air and I'm having trouble figuring out what my chamber temperature would be. I understand in this case it would be the temperature of the gas before entering the nozzle but I'm not sure if that would just be ambient temperature, same as exit temperature (ambient temperature) or something else. I'm trying to find my chamber temperature so I can calculate my exit velocity and thrust.