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Overview of RS-25 Adaptation Hot-Fire Test Series for SLS, Status and Lessons LearnedThis paper discusses the engine system design, hot-fire test history and analyses for the RS-25 Adaptation Engine test series, a major hot-fire test series supporting the Space Launch System (SLS) program. The RS-25 is an evolution of the Space Shuttle Main Engine (SSME). Since the SLS mission profile and engine operating conditions differ from that experienced by the SSME, a test program was needed to verify that SLS-unique requirements could be met by the adapted legacy engines. A series of 18 tests, including one engine acceptance test, was conducted from January 2015 to October 2017, to directly support Exploration Mission-1 (EM-1), the first flight of SLS. These tests were the first hot-firings of legacy SSME hardware since 2009. Major findings are described along with top level overview of the engine system.
Document ID
20180006338
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Vetcha, Naveen
(Jacobs Technology, Inc. Huntsville, AL, United States)
Strickland, Matthew B.
(Jacobs Technology, Inc. Huntsville, AL, United States)
Philippart, Kenneth D.
(Jacobs Technology, Inc. Huntsville, AL, United States)
Giel, Thomas V., Jr.
(Jacobs Technology, Inc. Huntsville, AL, United States)
Date Acquired
October 17, 2018
Publication Date
July 9, 2018
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
M18-6787
Meeting Information
Meeting: AIAA Propulsion and Energy Forum
Location: Cincinnati, OH
Country: United States
Start Date: July 9, 2018
End Date: July 11, 2018
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: 80MSFC18C0011
Distribution Limits
Public
Copyright
Public Use Permitted.
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