DocumentCode :
1878915
Title :
Mars Sample Return campaign status
Author :
Nilsen, Erik ; Whetsel, Charles ; Mattingly, Richard ; May, Lisa
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
fYear :
2012
fDate :
3-10 March 2012
Firstpage :
1
Lastpage :
7
Abstract :
The proposed Mars Sample Return (MSR) Campaign would be the next big step in the Mars Exploration Program (MEP). Identified by the Planetary Decadal Survey of 2011 as the highest science priority for large missions, the Mars Program has been working in partnership with the European Space Agency (ESA) to define a campaign to return a surface sample of martian surface material to Earth for analysis. As currently envisioned, the MSR campaign concept consists of a series of flight missions to collect and return the sample, and a ground based project to develop a sample receiving facility. The first mission in this proposed campaign would be baselined for launch in 2018, and would consist of a rover capable of scientifically selecting and caching the sample for retrieval by a later mission. Subsequent missions would retrieve the cache, launch it into orbit around Mars, where it would be captured by an orbiter and returned to the Earth. This paper discusses the current status of the MSR Campaign architecture definition and requirements development and near term plans for technical definition and review. Also discussed are selected design drivers and proposed key requirements which would have to be addressed in the definition of the campaign.1, 2
Keywords :
Mars; artificial satellites; astronomical instruments; planetary surfaces; European Space Agency; Mars exploration program; Mars sample return campaign; architecture definition; martian surface material; requirements development; Earth; Investments; Mars; NASA; Orbits; Surface topography; Surface treatment;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2012 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
978-1-4577-0556-4
Type :
conf
DOI :
10.1109/AERO.2012.6187032
Filename :
6187032
Link To Document :
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