From Concept to Flight: An Active Fluid Loop Based Thermal Control System for Mars Science Laboratory Rover
Author:
Affiliation:
1. Jet Propulsion Laboratory, California Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-3514
Reference21 articles.
1. Integrated Pump Assembly - An Active Cooling System for Mars Pathfinder Thermal Control
2. 3Birur, G. and P. Bhandari, "Mars Pathfinder Active Thermal Control System: Ground and Flight Performance of a MechanicallyPumped Loop,"Paper No AIAA-97-2469,32ndThermophysicsConference,Atlanta,GA,June23-25,1997.
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