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NASA's Space Launch System: An Evolving Capability for Exploration An Evolving Capability for ExplorationA foundational capability for international human deep-space exploration, NASA's Space Launch System (SLS) vehicle represents a new spaceflight infrastructure asset, creating opportunities for mission profiles and space systems that cannot currently be executed. While the primary purpose of SLS, which is making rapid progress towards initial launch readiness in two years, will be to support NASA's Journey to Mars, discussions are already well underway regarding other potential utilization of the vehicle's unique capabilities. In its initial Block 1 configuration, capable of launching 70 metric tons (t) to low Earth orbit (LEO), SLS is capable of propelling the Orion crew vehicle to cislunar space, while also delivering small CubeSat-class spacecraft to deep-space destinations. With the addition of a more powerful upper stage, the Block 1B configuration of SLS will be able to deliver 105 t to LEO and enable more ambitious human missions into the proving ground of space. This configuration offers opportunities for launching co-manifested payloads with the Orion crew vehicle, and a class of secondary payloads, larger than today's CubeSats. Further upgrades to the vehicle, including advanced boosters, will evolve its performance to 130 t in its Block 2 configuration. Both Block 1B and Block 2 also offer the capability to carry 8.4- or 10-m payload fairings, larger than any contemporary launch vehicle. With unmatched mass-lift capability, payload volume, and C3, SLS not only enables spacecraft or mission designs currently impossible with contemporary EELVs, it also offers enhancing benefits, such as reduced risk, operational costs and/or complexity, shorter transit time to destination or launching large systems either monolithically or in fewer components. This paper will discuss both the performance and capabilities of Space Launch System as it evolves, and the current state of SLS utilization planning.
Document ID
20160012112
Acquisition Source
Marshall Space Flight Center
Document Type
Abstract
Authors
Creech, Stephen D.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Crumbly, Christopher M.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Robinson, Kimerly F.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
October 7, 2016
Publication Date
September 26, 2016
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
M16-5115
Report Number: M16-5115
Meeting Information
Meeting: International Astronautical Congress: Session D2.8 Going To and Beyond the Earth-Moon System: Human Missions to Mars, Libration Points and NEO''s
Location: Guadalajara
Country: Mexico
Start Date: September 26, 2016
End Date: September 30, 2016
Sponsors: International Astronautical Federation
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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