Mars design reference mission: Difference between revisions
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The Mars design reference mission is a series of missions plans that have been regularly updated by NASA. The current version is version 5<ref>https://en.wikipedia.org/wiki/Mars_Design_Reference_Mission</ref>. | The Mars design reference mission is a series of missions plans that have been regularly updated by NASA. The current version is version 5<ref>https://en.wikipedia.org/wiki/Mars_Design_Reference_Mission</ref>. | ||
=== References === | History | ||
* Version 1 1993. Based on Mars direct. 900 tonnes mission. Crew of six. | |||
* Version 2 1997. | |||
* Version 3 1998. Reduced system mass, smaller launchers. 450 tonnes mission. | |||
* Version 4 1998. Explored Nuclear thermal and electric propulsion variants | |||
* Version 5 2009<ref>https://www.nasa.gov/pdf/373665main_NASA-SP-2009-566.pdf</ref>. Addendum 2, 2014<ref>https://www.nasa.gov/sites/default/files/files/NASA-SP-2009-566-ADD2.pdf</ref>. Ares V. | |||
===References=== | |||
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Revision as of 13:07, 11 June 2019
The Mars design reference mission is a series of missions plans that have been regularly updated by NASA. The current version is version 5[1].
History
- Version 1 1993. Based on Mars direct. 900 tonnes mission. Crew of six.
- Version 2 1997.
- Version 3 1998. Reduced system mass, smaller launchers. 450 tonnes mission.
- Version 4 1998. Explored Nuclear thermal and electric propulsion variants
- Version 5 2009[2]. Addendum 2, 2014[3]. Ares V.