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Thermal Modeling of Mars Ground for Surface MissionsThermal analysis packages are capable of including ground temperature effects for orbital and surface thermal analyses. In particular, Thermal Desktop® offers the option of specifying ground temperatures as a function of time for planetary surface modeling. While suitable for many cases, this approach is not sufficient if an object has local interactions with the ground that could significantly affect the ground temperature. Ground modeling is necessary for the Mars 2020 rover thermal design and analysis since shadowing and heat dissipation from the rover’s Multi-Mission Radioisotope Thermoelectric Generator (MMRTG) can result in significant temperature deviations of the local ground. The Mars 2020 thermal team is explicitly modeling the Martian ground so that these local temperature effects can be captured. The upper portion of the ground is modeled, and material and optical properties of the ground are varied in order to match data collected from orbiting science instruments. Atmospheric surface temperature, sky temperatures, and solar loads from a Mars General Circulation Model (GCM) are used as boundary conditions, resulting in a ground surface temperature profile consistent with the GCM predictions. The rover model is then placed on this modeled ground so that the effects of shadowing and MMRTG dissipation on the ground temperature can be captured.
Document ID
20190028471
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Farias, Edgardo
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Redmond, Matthew
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Bhandari, Pradeep
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Kempenaar, Jason
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Novak, Keith
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 1, 2019
Publication Date
July 16, 2017
Subject Category
Ground Support Systems And Facilities (Space)
Lunar And Planetary Science And Exploration
Report/Patent Number
JPL-CL-CL#17-2091
ICES-2017-198
Report Number: JPL-CL-CL#17-2091
Report Number: ICES-2017-198
Meeting Information
Meeting: International Conference on Environmental Systems (ICES 2017)
Location: Charleston, SC
Country: United States
Start Date: July 16, 2017
End Date: July 20, 2017
Sponsors: International Conference On Environmental Systems, Inc.
Distribution Limits
Public
Copyright
Other

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