DocumentCode
2787486
Title
Mars human precursor mission concepts for the decade 2010-2020
Author
Andringa, Jason M. ; Easter, Robert W. ; Gray, Andrew A. ; Lamassoure, Elisabeth S. ; Mungas, Greg S.
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., USA
fYear
2005
fDate
5-12 March 2005
Firstpage
191
Lastpage
201
Abstract
In the president´s vision for space exploration presented in January 2004, a human precursor test bed mission series is identified for both the Moon and Mars. It is assumed that the test bed missions to Mars will satisfy measurement recommendations from the Mars human precursor science steering group (MHP SSG), the Mars exploration program analysis group (MEPAG), and the National Research Council´s (NRC) Safe on Mars report. Technology demonstrations and technology feed-forward such as heavy landing, hazard avoidance, pinpoint landing, and in-situ resource utilization (ISRU) must also be accomplished. A number of concepts to complete such tasks have been developed by the pre-projects and Advanced Studies Office at the Jet Propulsion Laboratory (JPL). Concepts for orbiters, single stationary or mobile landers, and multiple stationary or mobile landers have been developed. This paper provides an overview of the concepts developed to date to satisfy human precursor measurements and demonstrations.
Keywords
Mars; aerospace safety; human factors; space vehicles; Advanced Studies Office; ISRU; Jet Propulsion Laboratory; MEPAG; MHP SSG; Mars exploration program analysis group; Mars human precursor science steering group; Moon; National Research Council Safe; hazard avoidance; heavy landing; human precursor mission; in-situ resource utilization; mobile landers; pinpoint landing; space exploration; test bed mission; Extraterrestrial measurements; Feedforward systems; Hazards; Humans; Mars; Moon; Propulsion; Resource management; Space exploration; Testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2005 IEEE
Conference_Location
Big Sky, MT
Print_ISBN
0-7803-8870-4
Type
conf
DOI
10.1109/AERO.2005.1559312
Filename
1559312
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