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Space Shuttle Main Engine /SSME/ - The 'maturing' processThe basic Space Shuttle Main Engine (SSME) concept called for an operational life of 55 missions, as well as an exceptionally high specific impulse. While these requirements are considered achievable in the cases of the basic engine structure, powerhead, main combustion chamber, propellant ducts, hydraulic lines and engine controller, other components may experience excessive wear and deterioration and may not achieve specification life without removal and overhaul. Most SSME components have been designed as line replaceable units, which have demonstrated good operational durability and will meet flight certification requirement upgrading. The Flight Confidence Program of the SSME test program currently being instituted will recertify existing engines for use in more than the 10 flights stipulated until now. The testing of two engines in repeated cycles should add 10 flights for every two successfully completed certification cycles.
Document ID
19830037591
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Dankhoff, W.
(NASA Headquarters Washington, DC United States)
Mcilwain, M. C.
(NASA Office of Space Transportation Systems Washington, DC, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Publication Information
Publication: Astronautics and Aeronautics
Volume: 21
Subject Category
Spacecraft Propulsion And Power
Accession Number
83A18809
Distribution Limits
Public
Copyright
Other

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