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NASA's Space Launch System Moves into Testing and IntegrationNASA's Space Launch System (SLS) has moved from design and manufacturing into testing and integration for its first flight in fiscal year 2020. In 2017, the NASA/industry team completed manufacturing of all major structural elements for the launch vehicle for Exploration Mission-1 (EM-1). This work included shipping the first major flight hardware element to the launch site. Current work is focused on the initial Block 1 variant of SLS, capable of launching more than 70 metric tons (t) to low Earth orbit (LEO). As the needs of the nation's deep space exploration program grow, SLS performance is designed to evolve to a payload mass of 130 t to LEO and up to 45 metric tons (t) to trans-lunar injection (TLI). The advantages of this mass - as well as volume - are critical to the entire exploration architecture for deep space exploration. They translate to greater capability, greater infrastructure and operational simplicity, less overall mission risk, and opportunities to accomplish unprecedented exploration and discovery.
Document ID
20180007875
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Honeycutt, John
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Creech, Steve
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
November 27, 2018
Publication Date
October 1, 2018
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
IAC-18-D2.1
M18-6977
Report Number: IAC-18-D2.1
Report Number: M18-6977
Meeting Information
Meeting: International Astronautical Congress (IAC 2018)
Location: Bremen
Country: Germany
Start Date: October 1, 2018
End Date: October 5, 2018
Sponsors: Deutsches Zentrum fuer Luft- und Raumfahrt e.V.
Funding Number(s)
CONTRACT_GRANT: NM07AA70C
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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