One method to reduce the cost of space missions is to launch them on smaller, less expensive launch vehicles. This requires smaller and lighter spacecraft. For a Mars sample return mission concept under consideration, the method to achieve this is to use indigenous Martian carbon dioxide, combined w
Cryogenic propellant liquefaction and storage for a precursor to a human Mars mission
✍ Scribed by P. Mueller; T. Durrant
- Publisher
- Elsevier Science
- Year
- 1999
- Tongue
- English
- Weight
- 290 KB
- Volume
- 39
- Category
- Article
- ISSN
- 0011-2275
No coin nor oath required. For personal study only.
✦ Synopsis
An analysis of cryogenic liquefaction and storage methods for in-situ produced propellants (oxygen and methane) on Mars is presented. The application is to a subscale precursor sample return mission, intended to demonstrate critical cryogenic technologies prior to a human mission. A heat transfer analysis is included, resulting in predicted cryogenic tank surface temperatures and heat leak values for dierent conditions. Insulation thickness is traded o against cryocooler capacity to ®nd optimum combinations for various insulation con®gurations, including multilayer insulation and microspheres. Microsphere insulation is shown to have promise, and further development is recommended.
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