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Thermal Response of the Mars Science Laboratory Spacecraft During Entry, Descent and LandingNASA’s Mars Science Laboratory (MSL) spacecraft successfully performed its Entry, Descent & Landing (EDL) phase on August 6, 2012. This paper presents the thermal response of the MSL spacecraft from EDL Initialization (5 days prior to Entry) to Rover touchdown on the surface of Mars. Temperature telemetry recorded during EDL is used to reconstruct the thermal response of the spacecraft to each EDL event. Temperature profiles for the Descent Stage and Rover hardware are presented and explained in the context of the changing EDL environments (aerothermal heating and convective cooling) and power states.
Document ID
20190025577
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Novak, Keith S.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Miller, Jennifer R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Paris, Anthony D.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Kelly, Frank P.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
June 3, 2019
Publication Date
July 10, 2016
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
JPL-CL-16-1805
Report Number: JPL-CL-16-1805
Meeting Information
Meeting: International Conference on Environmental Systems
Location: Vienna
Country: Austria
Start Date: July 10, 2016
End Date: July 14, 2016
Sponsors: International Conference On Environmental Systems, Inc.
Distribution Limits
Public
Copyright
Other

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