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SSME Engine Controller Development and EvolutionThe SSME engine controller is a redundant, micro-processor based control unit. The controller along with its embedded software provides closed loop control of the engine s thrust and mixture ratio during flight as well as configuring the engine state and operations during non-flight activities such as checkouts, and pre-start engine conditioning. It processes orbiter commands into engine actions and provides engine state and health information to the orbiter for immediate action, telemetry and recording. In addition the controller includes functions which continually monitor and manage engine health, and can activate a variety of fault mitigation actions to insure safe engine operation. The objective of this paper is to provide a description of the SSME engine controller as well as its developmental history and lessons learned
Document ID
20100022134
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Abrams, Russ
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Moyers, Ronda
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Horne, Charles
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Bouffard, Marc
(Pratt and Whitney Rocketdyne Canoga Park, CA, United States)
Schuldt, Theodore, Jr.
(Pratt and Whitney Rocketdyne Canoga Park, CA, United States)
Date Acquired
August 24, 2013
Publication Date
May 3, 2010
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
M10-0260
Meeting Information
Meeting: 57th JANNAF Joint Propulsion Conference
Location: Colorado Springs, CO
Country: United States
Start Date: May 3, 2010
End Date: May 7, 2010
Sponsors: NASA Headquarters, Department of the Navy, Department of the Air Force, Department of the Army
Distribution Limits
Public
Copyright
Other

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