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Assessment of Environments for Mars Science Laboratory Entry, Descent, and Surface Operations

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Abstract

The Mars Science Laboratory mission aims to land a car-sized rover on Mars’ surface and operate it for at least one Mars year in order to assess whether its field area was ever capable of supporting microbial life. Here we describe the approach used to identify, characterize, and assess environmental risks to the landing and rover surface operations. Novel entry, descent, and landing approaches will be used to accurately deliver the 900-kg rover, including the ability to sense and “fly out” deviations from a best-estimate atmospheric state. A joint engineering and science team developed methods to estimate the range of potential atmospheric states at the time of arrival and to quantitatively assess the spacecraft’s performance and risk given its particular sensitivities to atmospheric conditions. Numerical models are used to calculate the atmospheric parameters, with observations used to define model cases, tune model parameters, and validate results. This joint program has resulted in a spacecraft capable of accessing, with minimal risk, the four finalist sites chosen for their scientific merit. The capability to operate the landed rover over the latitude range of candidate landing sites, and for all seasons, was verified against an analysis of surface environmental conditions described here. These results, from orbital and model data sets, also drive engineering simulations of the rover’s thermal state that are used to plan surface operations.

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Abbreviations

AGL:

Above Ground Level

EDL:

Entry, Descent, and Landing

GFDL:

Geophysical Fluid Dynamics Laboratory, Princeton University

IR:

Infrared

JPL:

Jet Propulsion Laboratory

MARCI:

Mars Color Imager

Mars-GRAM:

Mars Global Reference Atmospheric Model

MCS:

Mars Climate Sounder

MEP:

Mars Exploration Program

MER:

Mars Exploration Rover

MGCM:

Mars General Circulation Model

MGS:

Mars Global Surveyor

MOC:

Mars Orbiter Camera

MOLA:

Mars Orbiter Laser Altimeter

MMM5:

Mars Mesoscale Model 5

MPF:

Mars Pathfinder

MRAMS:

Mars Regional Atmospheric Modeling System

MRO:

Mars Reconnaissance Orbiter

MSL:

Mars Science Laboratory

MY:

Mars Year

NASA:

National Aeronautics and Space Administration

NMSU:

New Mexico State University

ODY:

Mars Odyssey

RS:

Radio Science

TES:

Thermal Emission Spectrometer

THEMIS:

Thermal Emission Imaging System

UKMGCM:

United Kingdom MGCM

UTC:

Coordinated Universal Time

VL:

Viking Lander

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Acknowledgements

Adam Steltzner, Steve Sell, Richard Powell, David Way, and Jody Davis were additional key contributors to the design and development of the MSL EDL system. Rich Zurek provided a watchful eye and helped secure a Mars Climate Sounder data campaign one Mars year before arrival. Charles Budney and Tommy Thompson administered the MEP Critical Data Products program that greatly enhanced the characterization efforts. Leila Lorenzoni helped lead the initial atmospheric safety assessment at JPL. Fred Calef III helped with GIS analyses of landing site surface temperatures. R. John Wilson and Mark Richardson contributed to the assembly of the JPL 1-D model. This research was carried out at the Jet Propulsion Laboratory, California Institute of Technology, under a contract with the National Aeronautics and Space Administration.

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Correspondence to Ashwin R. Vasavada.

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Vasavada, A.R., Chen, A., Barnes, J.R. et al. Assessment of Environments for Mars Science Laboratory Entry, Descent, and Surface Operations. Space Sci Rev 170, 793–835 (2012). https://doi.org/10.1007/s11214-012-9911-3

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  • DOI: https://doi.org/10.1007/s11214-012-9911-3

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