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Thermal Control System for a Small, Extended Duration Lunar Surface Science PlatformThe presentation slides include: Introduction: lunar mission definition, Problem: requirements/methodology, Concept: thermal switching options, Analysis: system evaluation, Plans: dual-radiator LHP (loop heat pipe) test bed, and Conclusions: from this study.
Document ID
20100017675
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Bugby, D. (ATK Launch Systems Huntsville, AL, United States)
Farmer, J. (NASA Marshall Space Flight Center Huntsville, AL, United States)
OConnor, B. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Wirzburger, M. (Johns Hopkins Univ. Laurel, MD, United States)
Abel, E. (Johns Hopkins Univ. Laurel, MD, United States)
Stouffer, C. (ATK Launch Systems Huntsville, AL, United States)
Date Acquired
August 24, 2013
Publication Date
March 9, 2010
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
M10-0336
Meeting Information
Meeting: Spacecraft Thermal COntrol Workshop
Location: El Segundo, CA
Country: United States
Start Date: March 9, 2010
End Date: March 11, 2010
Distribution Limits
Public
Copyright
Public Use Permitted.

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