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Main propulsion system test requirements for the two-engine Shuttle-CThe Shuttle-C is an unmanned cargo carrying derivative of the space shuttle with optional two or three space shuttle main engines (SSME's), whereas the shuttle has three SSME's. Design and operational differences between the Shuttle-C and shuttle were assessed to determine requirements for additional main propulsion system (MPS) verification testing. Also, reviews were made of the shuttle main propulsion test program objectives and test results and shuttle flight experience. It was concluded that, if significant MPS modifications are not made beyond those currently planned, then main propulsion system verification can be concluded with an on-pad flight readiness firing.
Document ID
19900004966
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Lynn, E. E.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Platt, G. K.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1989
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-TM-100382
NAS 1.15:100382
Accession Number
90N14282
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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