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NASA's Space Launch System (SLS) Program: Mars Program UtilizationNASA's Space Launch System is being designed for safe, affordable, and sustainable human and scientific exploration missions beyond Earth's orbit (BEO), as directed by the NASA Authorization Act of 2010 and NASA's 2011 Strategic Plan. This paper describes how the SLS can dramatically change the Mars program's science and human exploration capabilities and objectives. Specifically, through its high-velocity change (delta V) and payload capabilities, SLS enables Mars science missions of unprecedented size and scope. By providing direct trajectories to Mars, SLS eliminates the need for complicated gravity-assist missions around other bodies in the solar system, reducing mission time, complexity, and cost. SLS's large payload capacity also allows for larger, more capable spacecraft or landers with more instruments, which can eliminate the need for complex packaging or "folding" mechanisms. By offering this capability, SLS can enable more science to be done more quickly than would be possible through other delivery mechanisms using longer mission times.
Document ID
20120015287
Acquisition Source
Marshall Space Flight Center
Document Type
Extended Abstract
Authors
May, Todd A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Creech, Stephen D.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 26, 2013
Publication Date
June 12, 2012
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
M12-1765
Report Number: M12-1765
Meeting Information
Meeting: Concepts and Approaches for Mars Exploration at the Lunar and Planetary Institute
Location: Houston, TX
Country: United States
Start Date: June 12, 2012
End Date: June 14, 2012
Sponsors: Lunar and Planetary Inst.
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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