NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Space Shuttle Orbiter Reaction Jet Driver (RJD): Independent Technical Assessment/Inspection (ITA/I) Report, Version 1.0The Space Shuttle Program (SSP) has a zero-fault-tolerant design related to an inadvertent firing of the primary reaction control jets on the Orbiter during mated operations with the International Space Station (ISS). Failure modes identified by the program as a wire-to-wire "smart" short or a Darlington transistor short resulting in a failed-on primary thruster during mated operations with ISS can drive forces that exceed the structural capabilities of the docked Shuttle/ISS structure. The assessment team delivered 17 observations, 6 findings and 15 recommendations to the Space Shuttle Program.
Document ID
20050185209
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Gilbrech, Richard J.
(NASA Langley Research Center Hampton, VA, United States)
Kichak, Robert A.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Davis, Mitchell
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Williams, Glenn
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Thomas, Walter, III
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Slenski, George A.
(Department of the Air Force Wright-Patterson AFB, OH, United States)
Hetzel, Mark
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 7, 2013
Publication Date
March 1, 2005
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NESC-RP-05-18-Version-1.0
NASA/TM-2005-213750/VERSION1.0
L-19119/VERSION1.0
Report Number: NESC-RP-05-18-Version-1.0
Report Number: NASA/TM-2005-213750/VERSION1.0
Report Number: L-19119/VERSION1.0
Funding Number(s)
WORK_UNIT: WU 104-08-46
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available