Table 1 Optimization results
Stage | 6 stages maneuver | 10 stages maneuver | ||
|---|---|---|---|---|
\(\Delta v\) (in m/s) | Propellant Ratio | \(\Delta v\) (in m/s) | Propellant Ratio | |
Stage 1 (start) | 0 | 1.0000e+00 | 0 | 1.0000e+00 |
Stage 2 | 1.3360e+04 | 2.0938e+02 | 1.1538e+04 | 1.0100e+02 |
Stage 3 | 1.5420e+04 | 4.7731e+02 | 1.3951e+04 | 2.6514e+02 |
Stage 4 | 1.6397e+04 | 7.0539e+02 | 1.5140e+04 | 4.2659e+02 |
Stage 5 | 1.6995e+04 | 8.9599e+02 | 1.5880e+04 | 5.7356e+02 |
Stage 6 | 1.7609e+04 | 1.0574e+03 | 1.6397e+04 | 7.0539e+02 |
Stage 7 | – | – | 1.6785e+04 | 8.2370e+02 |
Stage 8 | – | – | 1.7089e+04 | 9.3037e+02 |
Stage 9 | – | – | 1.7336e+04 | 1.0271e+03 |
Stage 10 | – | – | 1.7542e+04 | 1.0357e+03 |