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Overview of the Altair Lunar Lander Thermal Control System DesignNASA's Constellation Program has been developed to successfully return humans to the Lunar surface by 2020. The Constellation Program includes several different project offices including Altair, which is the next generation Lunar Lander. The planned Altair missions are very different than the Lunar missions accomplished during the Apollo era. These differences have resulted in a significantly different thermal control system architecture. The current paper will summarize the Altair mission architecture and the various operational phases. In addition, the derived thermal requirements will be presented. The paper will conclude with a brief description of the thermal control system designed to meet these unique and challenging thermal requirements.
Document ID
20100017019
Acquisition Source
Johnson Space Center
Document Type
Other
Authors
Stephan, Ryan A.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2010
Subject Category
Lunar And Planetary Science And Exploration
Report/Patent Number
JSC-CN-20210
Meeting Information
Meeting: International Conference on Environmental Systems
Location: Barcelona
Country: Spain
Start Date: July 11, 2010
End Date: July 15, 2010
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 119103.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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