Research Article
A Numerical Study of Low-Thrust Limited Power Trajectories between Coplanar Circular Orbits in an Inverse-Square Force Field
Table 6
Consumption variable for Earth-Mars transfers.
| | | | | | | | | |
| |
1.5236 | 2.0
3.0
4.0
5.0 | 1.7743 × 10−1
4.4947 × 10−2
1.6051 × 10−2
7.2498 × 10−3 | 1.7434 × 10−1
4.4067 × 10−2
1.5889 × 10−2
7.3352 × 10−3 | 1.7434 × 10−1
4.4066 × 10−2
1.5889 × 10−2
7.3351 × 10−3 | 1.7434 × 10−1
4.4066 × 10−2
1.5889 × 10−2
7.3351 × 10−3 | 1.77
1.99
1.02
1.16 | 0.00
0.00
0.00
0.00 | 0.00
0.00
0.00
0.00 | 20.0
30.0
40.0
50.0 | 8.6591 × 10−4
5.7537 × 10−4
4.2991 × 10−4
3.4273 × 10−4 | 9.3232 × 10−4
6.1074 × 10−4
4.5311 × 10−4
3.6096 × 10−4 | 9.3151 × 10−4
6.1071 × 10−4
4.5296 × 10−4
3.6093 × 10−4 | 9.3158 × 10−4
6.1073 × 10−4
4.5299 × 10−4
3.6095 × 10−4 | 7.02
5.79
5.09
5.04 | 0.09
0.00
0.03
0.01 | 0.01
0.00
0.01
0.01 |
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