| タイトル | Mars Earth Return Vehicle (MERV) Propulsion Options |
| 本文（外部サイト） | http://hdl.handle.net/2060/20100029641 |
| 著者（英） | Hemminger, Joseph; Oleson, Steven R.; Williams, Glenn; Fittje, Jim; Martini, Mike; Gyekenyesi, John; Warner, Joe; Fincannon, James; Parkey, Thomas; Packard, Tom; McGuire, Melissa L.; Burke, Laura; Colozza, Tony |
| 著者所属（英） | NASA Glenn Research Center |
| 発行日 | 2010-07-25 |
| 言語 | eng |
| 内容記述 | The COMPASS Team was tasked with the design of a Mars Sample Return Vehicle. The current Mars sample return mission is a joint National Aeronautics and Space Administration (NASA) and European Space Agency (ESA) mission, with ESA contributing the launch vehicle for the Mars Sample Return Vehicle. The COMPASS Team ran a series of design trades for this Mars sample return vehicle. Four design options were investigated: Chemical Return /solar electric propulsion (SEP) stage outbound, all-SEP, all chemical and chemical with aerobraking. The all-SEP and Chemical with aerobraking were deemed the best choices for comparison. SEP can eliminate both the Earth flyby and the aerobraking maneuver (both considered high risk by the Mars Sample Return Project) required by the chemical propulsion option but also require long low thrust spiral times. However this is offset somewhat by the chemical/aerobrake missions use of an Earth flyby and aerobraking which also take many months. Cost and risk analyses are used to further differentiate the all-SEP and Chemical/Aerobrake options. |
| NASA分類 | Spacecraft Propulsion and Power |
| レポートNO | E-17423 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/250847 |
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