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.
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0.7270 | 2.0 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 |
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