NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Operationally Efficient Propulsion System Study (OEPSS) Data BookA fluid-dynamic, digital-transient computer model of an integrated, parallel propulsion system was developed for the CDC mainframe and the SUN workstation computers. Since all STME component designs were used for the integrated system, computer subroutines were written characterizing the performance and geometry of all the components used in the system, including the manifolds. Three transient analysis reports were completed. The first report evaluated the feasibility of integrated engine systems in regards to the start and cutoff transient behavior. The second report evaluated turbopump out and combined thrust chamber/turbopump out conditions. The third report presented sensitivity study results in staggered gas generator spin start and in pump performance characteristics.
Document ID
19980041374
Acquisition Source
Kennedy Space Center
Document Type
Other - Collected Works
Authors
Kemp, Victoria R.
(Rockwell International Corp. Canoga Park, CA United States)
Date Acquired
September 6, 2013
Publication Date
October 30, 1992
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA/CR-92-207443
NAS 1.26:207443
RI/RD90-149-Vol-8
Funding Number(s)
CONTRACT_GRANT: NAS10-11568
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available