Selection of the Mars Science Laboratory Landing Site

被引:157
|
作者
Golombek, M. [1 ]
Grant, J. [2 ]
Kipp, D. [1 ]
Vasavada, A. [1 ]
Kirk, R. [3 ]
Fergason, R. [3 ]
Bellutta, P. [1 ]
Calef, F. [1 ]
Larsen, K. [4 ]
Katayama, Y. [1 ,5 ]
Huertas, A. [1 ]
Beyer, R. [6 ]
Chen, A. [1 ]
Parker, T. [1 ]
Pollard, B. [1 ]
Lee, S. [1 ]
Sun, Y. [1 ,7 ]
Hoover, R. [1 ,8 ]
Sladek, H. [1 ,9 ]
Grotzinger, J. [7 ]
Welch, R. [1 ]
Dobrea, E. Noe [1 ,10 ]
Michalski, J. [1 ,10 ]
Watkins, M. [1 ]
机构
[1] CALTECH, Jet Prop Lab, Pasadena, CA 91109 USA
[2] Smithsonian Inst, Natl Air & Space Museum, Washington, DC 20560 USA
[3] US Geol Survey, Flagstaff, AZ 86001 USA
[4] Univ Colorado, Lab Atmospher & Space Phys, Boulder, CO 80309 USA
[5] Japan Aerosp Explorat Agcy, Lunar & Planetary Explorat Program Grp, Tokyo, Japan
[6] NASA, Ames Res Ctr, Moffett Field, CA 94035 USA
[7] CALTECH, Pasadena, CA 91125 USA
[8] Univ Colorado, Boulder, CO 80309 USA
[9] Univ Montana Western, Dillon, MT 59725 USA
[10] Planetary Sci Inst, Tucson, AZ 85719 USA
关键词
Landing sites; Mars; Surface materials; Surface characteristics; Mars Science Laboratory; EMISSION SPECTROMETER EXPERIMENT; SIZE-FREQUENCY DISTRIBUTIONS; ORBITER LASER ALTIMETER; MAWRTH-VALLIS REGION; THERMAL INERTIA; GALE-CRATER; MELAS-CHASMA; PHYSICAL-PROPERTIES; LAYERED DEPOSITS; TERRA MERIDIANI;
D O I
10.1007/s11214-012-9916-y
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
The selection of Gale crater as the Mars Science Laboratory landing site took over five years, involved broad participation of the science community via five open workshops, and narrowed an initial > 50 sites (25 by 20 km) to four finalists (Eberswalde, Gale, Holden and Mawrth) based on science and safety. Engineering constraints important to the selection included: (1) latitude (+/- 30A degrees) for thermal management of the rover and instruments, (2) elevation (<-1 km) for sufficient atmosphere to slow the spacecraft, (3) relief of < 100-130 m at baselines of 1-1000 m for control authority and sufficient fuel during powered descent, (4) slopes of < 30A degrees at baselines of 2-5 m for rover stability at touchdown, (5) moderate rock abundance to avoid impacting the belly pan during touchdown, and (6) a radar-reflective, load-bearing, and trafficable surface that is safe for landing and roving and not dominated by fine-grained dust. Science criteria important for the selection include the ability to assess past habitable environments, which include diversity, context, and biosignature (including organics) preservation. Sites were evaluated in detail using targeted data from instruments on all active orbiters, and especially Mars Reconnaissance Orbiter. All of the final four sites have layered sedimentary rocks with spectral evidence for phyllosilicates that clearly address the science objectives of the mission. Sophisticated entry, descent and landing simulations that include detailed information on all of the engineering constraints indicate all of the final four sites are safe for landing. Evaluation of the traversabilty of the landing sites and target "go to" areas outside of the ellipse using slope and material properties information indicates that all are trafficable and "go to" sites can be accessed within the lifetime of the mission. In the final selection, Gale crater was favored over Eberswalde based on its greater diversity and potential habitability.
引用
收藏
页码:641 / 737
页数:97
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