Overview of RS-25 Adaptation Hot-Fire Test Series for SLS, Status and Lessons Learned
Author(s) -
Naveen Vetcha,
Matthew B. Strickland,
Kenneth D. Philippart,
T.V. Giel
Publication year - 2018
Publication title -
2018 joint propulsion conference
Language(s) - English
Resource type - Conference proceedings
SCImago Journal Rank - 0.242
H-Index - 10
DOI - 10.2514/6.2018-4459
Subject(s) - adaptation (eye) , space shuttle , test (biology) , aeronautics , series (stratigraphy) , engineering , aerospace engineering , computer science , simulation , paleontology , physics , optics , biology
This 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.
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