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Thermal Design and Flight Experience of the Mars Exploration Rover Spacecraft Computer-Controlled, Propulsion Line HeatersThe viewgraph presentation examines propulsion line heater design and problems in the Mars Rover. Topics include a Mars Exploration Rover (MER) project description and MER spacecraft configuration, mission overview, MER cruise stage hardware, thermal design drivers in the propulsion lines, propulsion line control set points prior to launch, MER A and B flight trajectories, MER A early and mid cruise flight experience, MER A and B mid cruise flight experience, MER B late cruise flight experience, and lessons learned
Document ID
20070038979
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Novak, Keith
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Kinsella, Gary
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Krylo, Robert
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Sunada, Eric
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 24, 2013
Publication Date
July 21, 2004
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: 34th International Conference on Environmental Systems (ICES)
Location: Colorado Springs, CO
Country: United States
Start Date: July 19, 2004
End Date: July 22, 2004
Distribution Limits
Public
Copyright
Other
Keywords
propulsion lines
thermal designs
Mars Exploration Rover
heaters

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