Optimal Spacecraft Trajectories for Flight to Asteroid Apophis With Return to Earth Using Chemical High Thrust Engines (IAA-AAS-DyCoSS2-14-15-02 — AAS 14-606)
Proceedings of the 2nd International Academy of Astronautics Conference on Dynamics and Control of Space Systems (DyCoSS)
01.01.2015
16 pages
Aufsatz (Konferenz)
Englisch
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