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Space Launch System Engine Out CapabilitiesNASA's SLS is being developed with the primary purpose of returning people to the Moon and eventually landing people on Mars. With these lofty goals, ensuring mission completion is paramount even in the event of an in-flight mishap. One possible mishap is the loss of an engine in flight. While SLS was not required to show full engine out capability, the program took an ``assess to'' approach to see when the launch vehicle could complete the mission after an engine failure versus when the launch vehicle targets required a down-mode to an alternate mission target to ensure at least some flight objectives were complete, or at a minimum ensure safe return of Orion and the Crew. While this paper will focus on Artemis I, an uncrewed mission, some comparisons will be made to how the engine out capability will change for the subsequent Crewed flights of SLS and Orion.
Document ID
20205004525
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
A. S. Craig
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
M. J. Hawkins
(Jacobs (United States) Dallas, Texas, United States)
J. E. Hauglie
(Jacobs (United States) Dallas, Texas, United States)
J. J. Hays
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Date Acquired
July 16, 2020
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
AAS 20-589
Meeting Information
Meeting: 2020 AAS/AIAA Astrodynamics Specialist Conference
Location: Virtual
Country: US
Start Date: August 9, 2020
End Date: August 13, 2020
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 585777.02.20.04.02.10
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Space Launch System
SLS
Engine Out
Guidance
Trajectory Optimization
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