DocumentCode :
2291445
Title :
Mars Sample Return a robust mission approach for "getting the right sample"
Author :
Evanyo, John A. ; Delamere, Alan ; Gulick, Doug ; Horsley, Bill ; Fischer, Cherissa ; Mann, Diana ; Miller, Kevin ; Mitchell, Scott ; Svitek, Tomas ; Padavano, Joseph ; Whittaker, Red ; Uphoff, Chauncey ; Helleckson, Brent ; Loucks, Mike ; Boynton, John ;
Author_Institution :
Ball Aerosp. Syst. Group, Boulder, CO, USA
Volume :
2
fYear :
2002
fDate :
2002
Firstpage :
2
Abstract :
The Mars Sample Return (MSR) mission plans to collect a set of soil samples from the Martian surface and return them to Earth for detailed analysis. The NASA Jet Propulsion Laboratory funded a series of industry led studies in 2001 to investigate the alternatives for the MSR mission. The results of this and previous studies indicate that a Mars sample return mission is feasible with available technologies. The Ball MSR study focused on several key objectives to provide a solid framework for the mission including: (1) a strong emphasis on science and "getting the right sample"; (2) a robust mission architecture to provide greater reliability and to reduce risk; (3) isotope powered autonomous rovers to support ambitious science objectives; (4) enhanced landing systems to improve landing accuracy and to provide direct access to the areas of highest scientific interest; (5) a quarantine of the returned sample in Earth orbit and retrieval by a separate mission with a containment vault to prevent inadvertent release of the sample into the Earth\´s biosphere.
Keywords :
Mars; space vehicles; Ball Aerospace; MSR mission; Mars Sample Return; Martian surface sample; available technologies; containment vault; isotope powered autonomous rovers; landing accuracy; landing systems; quarantine; reliability; robust mission architecture; Earth; Geoscience; Laboratories; Mars; NASA; Power system reliability; Propulsion; Robustness; Soil; Space technology;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference Proceedings, 2002. IEEE
Print_ISBN :
0-7803-7231-X
Type :
conf
DOI :
10.1109/AERO.2002.1035556
Filename :
1035556
Link To Document :
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