| タイトル | Lifting Mechanism for the Mars Explorer Rover |
| 本文（外部サイト） | http://hdl.handle.net/2060/20110016289 |
| 著者（英） | Harrington, Brian; Voorhees, Christopher; Melko, Joseph; Iskenderian, Theodore |
| 著者所属（英） | California Inst. of Tech. |
| 発行日 | 2005-10-01 |
| 言語 | eng |
| 内容記述 | A report discusses the design of a rover lift mechanism (RLM) -- a major subsystem of each of the Mars Exploration Rover vehicles, which were landed on Mars in January 2004. The RLM had to satisfy requirements to (1) be foldable as part of an extremely dense packing arrangement and (2) be capable of unfolding itself in a complex, multistep process for disengaging the rover from its restraints in the lander, lifting the main body of the rover off its landing platform, and placing the rover wheels on the platform in preparation for driving the rover off the platform. There was also an overriding requirement to minimize the overall mass of the rover and lander. To satisfy the combination of these and other requirements, it was necessary to formulate an extremely complex design that integrated components and functions of the RLM with those of a rocker-bogie suspension system, the aspects of which have been described in several prior NASA Tech Briefs articles. In this design, suspension components also serve as parts of a 4- bar linkage in the RLM. |
| NASA分類 | Spacecraft Design, Testing and Performance |
| レポートNO | NPO-40875 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/269353 |
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