Research Article

A Numerical Study of Low-Thrust Limited Power Trajectories between Coplanar Circular Orbits in an Inverse-Square Force Field

Table 5

Consumption variable for Earth-Venus transfers.


0.72702.0
3.0
4.0
5.0
3.7654 × 10−2
8.9269 × 10−3
4.0482 × 10−3
2.8941 × 10−3
3.7299 × 10−2
9.0261 × 10−3
4.2133 × 10−3
3.0573 × 10−3
3.7298 × 10−2
9.0259 × 10−3
4.2131 × 10−3
3.0572 × 10−3
3.7298 × 10−2
9.0259 × 10−3
4.2131 × 10−3
3.0572 × 10−3
0.95
1.10
3.91
5.33
0.00
0.00
0.00
0.00
0.00
0.00
0.00
0.00
20.0
30.0
40.0
50.0
7.2355 × 10−4
4.8236 × 10−4
3.6177 × 10−4
2.8942 × 10−4
7.4857 × 10−4
4.9863 × 10−4
3.7385 × 10−4
2.9903 × 10−4
7.4856 × 10−4
4.9862 × 10−4
3.7384 × 10−4
2.9901 × 10−4
7.4856 × 10−4
4.9862 × 10−4
3.7383 × 10−4
2.9897 × 10−4
3.34
3.26
3.22
3.20
0.00
0.00
0.00
0.01
0.00
0.00
0.00
0.01