any ideas?
If 90% of the initial mass is propellant, then M_f/M_i is 0.1, not 0.9.0.9 = e^(-deltaV / 4000)
0.9 = e^(-deltaV / 40,000)
Solve for delta V
Case 1, I got 421.442 m/s.
Case 2, I got 4214.421 m/s.
If 90% of the initial mass is propellant, then M_f/M_i is 0.1, not 0.9.
Case 1, I got 9210.340 m/s.
Case 2, I got 92103.404 m/s.
Edit: First time I did it, I used Mfinal / Minitial = 0.9, but that doesn't make sense since the propellant is burned off leaving 10% of the initial mass left. But the delta V sounds really high, so take my solution with a grain of salt.
Jesus, how the **** can you guys understand all this???