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SLS Evolution: Comparing Configurations Using System ExergyA human mission to the moon and Mars is the stated space exploration goal of the United States and the international community. To achieve these goals, NASA is developing the Space Launch System (SLS) and the Orion crew capsule as key elements in the architecture for missions to the moon and Mars. SLS will continue to evolve, adding capability that will further aid the missions to the moon and Mars. This paper examines the various configurations of SLS using energy analysis.
Document ID
20205008000
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Terry Hawes
(Northrop Grumman (United States) Falls Church, Virginia, United States)
Joshua Zimmerman
(Northrop Grumman (United States) Falls Church, Virginia, United States)
Michael Edward Fuller
(Northrop Grumman (United States) Falls Church, Virginia, United States)
Michael Watson
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Date Acquired
September 24, 2020
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: AIAA ASCEND
Location: Online
Country: US
Start Date: November 16, 2020
End Date: November 18, 2020
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNM07AA75C
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
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