| タイトル | Mars Hybrid Propulsion System Trajectory Analysis |
| 本文（外部サイト） | http://hdl.handle.net/2060/20160006327 |
| 著者（英） | Chai, Patrick R.; Qu, Min; Merrill, Raymond G. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2015-08-31 |
| 言語 | eng |
| 内容記述 | NASA's Human Spaceflight Architecture Team is developing a reusable hybrid transportation architecture in which both chemical and electric propulsion systems are used to send crew and cargo to Mars destinations such as Phobos, Deimos, the surface of Mars, and other orbits around Mars. By combining chemical and electrical propulsion into a single spaceship and applying each where it is more effective, the hybrid architecture enables a series of Mars trajectories that are more fuel-efficient than an all chemical architecture without significant increases in flight times. This paper shows the feasibility of the hybrid transportation architecture to pre-deploy cargo to Mars and Phobos in support of the Evolvable Mars Campaign crew missions. The analysis shows that the hybrid propulsion stage is able to deliver all of the current manifested payload to Phobos and Mars through the first three crew missions. The conjunction class trajectory also allows the hybrid propulsion stage to return to Earth in a timely fashion so it can be reused for additional cargo deployment. The 1,100 days total trip time allows the hybrid propulsion stage to deliver cargo to Mars every other Earth-Mars transit opportunity. For the first two Mars surface mission in the Evolvable Mars Campaign, the short trip time allows the hybrid propulsion stage to be reused for three round-trip journeys to Mars, which matches the hybrid propulsion stage's designed lifetime for three round-trip crew missions to the Martian sphere of influence. |
| NASA分類 | Space Transportation and Safety |
| レポートNO | NF1676L-20723 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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