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Preliminary Assessment of Mars Exploration Rover Landing Site PredictionsSelection of the Mars Exploration Rover (MER) landing sites took place over a three year period in which engineering constraints were identified, 155 possible sites were downselected to the final two, surface environments and safety considerations were developed, and the potential science return at the sites was considered. Landing sites in Gusev crater and Meridiani Planum were selected because they appeared acceptably safe for MER landing and roving and had strong morphologic and mineralogical indicators of liquid water in their past and thus appeared capable of addressing the science objectives of the MER missions, which are to determine the aqueous, climatic, and geologic history of sites on Mars where conditions may have been favorable to the preservation of evidence of possible pre-biotic or biotic processes. Engineering constraints important to the selection included: latitude (10 N-15 S) for maximum solar power; elevation (<-1.3 km) for sufficient atmosphere to slow the lander; low horizontal winds, shear and turbulence in the last few kilometers to minimize horizontal velocity; low 10-m scale slopes to reduce airbag spinup and bounce; moderate rock abundance to reduce abrasion or stroke-out of the airbags; and a radar-reflective, load-bearing and trafficable surface safe for landing and roving that is not dominated by fine-grained dust. In selecting the MER landing sites these engineering constraints were addressed via comprehensive evaluation of surface and atmospheric characteristics from existing remote sensing data and models as well as targeted orbital information acquired from Mars Global Surveyor and Mars Odyssey. This evaluation resulted in a number of predictions of the surface characteristics of the sites, which are tested in this abstract. Relating remote sensing signatures to surface characteristics at landing sites allows these sites to be used as ground truth for the orbital data, is essential for selecting and validating landing sites for future missions, and is required for correctly interpreting the surfaces and materials globally present on Mars.
Document ID
20040058002
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Golombek, M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Grant, J.
(Smithsonian Institution Washington, DC, United States)
Parker, T.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Crisp, J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Squyres, S.
(Cornell Univ. Ithaca, NY, United States)
Carr, M.
(Geological Survey Menlo Park, CA, United States)
Haldemann, A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Arvidson, R.
(Washington Univ. Saint Louis, MO, United States)
Ehlmann, B.
(Washington Univ. Saint Louis, MO, United States)
Bell, J.
(Cornell Univ. Ithaca, NY, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2004
Publication Information
Publication: Lunar and Planetary Science XXXV: Mars Missions
Subject Category
Lunar And Planetary Science And Exploration
Distribution Limits
Public
Copyright
Public Use Permitted.
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