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ROCKETS.py calculates the rocket fomura on TI-84 Python. Prompt Rocket Equation Solver Delta-v: 5,540 m/s Thrust: 2,278 kN Isp: 350 s Initial mass (m0): 12,550 kg Final mass (mf): 2,500 kg Burn time: ...
Also, I should probably check and make sure this model agrees with the classical rocket equation for a large number of fuel shots. Here is a plot of velocity vs. time for a five shot, 50 shot, and ...
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