Spiral escape trajectories enable a spacecraft to escape Earth’s gravity and travel into inter-planetary space under its own power. This analysis demonstrates how to design spiral escape trajectories that leverage single and double Lunar gravity assists and compares the effectiveness of each trajectory type. The trajectories are constructed by combining backwards propagated Q-Law and a perturbed Sims-Flanagan transcription to design the spiral and interplanetary phases, respectively. We demonstrate that these mission types result in significant propellant savings when compared to a conventional, no Lunar swingby spiral escape, and are highly beneficial for the interplanetary rideshare mission concept.
Exploration of Low-Thrust Lunar Swingby Escape Trajectories
31st Space Flight Mechanics Meeting ; 2021 ; Charlotte, NC, US
Conference paper
No indication
English
Optimal Lunar Swingby Trajectories
Online Contents | 2007
|Optimal lunar swingby trajectories
Online Contents | 2007
|Optimal lunar swingby trajectories
Springer Verlag | 2007
|Optimization of Solar-Perturbed Double Lunar Swingby Escape Trajectories
British Library Conference Proceedings | 1998
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