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NASA's Space Launch System: Progress Toward the Proving GroundSpace Launch System will be able to offer payload accommodations with five times more volume than any contemporary launch vehicle. center dot Payload fairings of up to 10-meter diameter are planned. Space Launch System will offer an initial capability of greater than 70 metric tons to low Earth orbit; current U.S. launch vehicle maximum is 28 t. center dot Evolved version of SLS will offer greatest-ever capability of greater than 130 t to LEO. SLS offers reduced transit times to the outer solar system by half or greater. center dot Higher characteristic energy (C3) also enables larger payloads to destination.
Document ID
20170008149
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Jackman, Angie
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 31, 2017
Publication Date
June 27, 2017
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
M17-6094
Report Number: M17-6094
Meeting Information
Meeting: IAA Symposium on the Future of Space Exploration Towards Space Village and Beyond
Location: Turin
Country: Italy
Start Date: June 27, 2017
End Date: June 29, 2017
Sponsors: International Academy of Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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