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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2021
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Article
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Tab 2
/
Research Article
Multiphase Trajectory Optimization of a Lunar Return Mission to an LEO Space Station
Table 2
Solutions for ETOs.
Design parameter
Optimal value
11030.9310
39.2871
-0.6291
19 April 2028 19:8:31.3362
181.96
3.20