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Shuttle cryogenic supply system optimization study. Volume 5A-2: Users manual for Space shuttle orbit injection system analysis (SOPSA)SOPSA (Shuttle Orbit Injection Propulsion System Analysis) is a computer program to aid in the preliminary design of propellant feed systems for the space shuttle orbiter main engines. The primary purpose of the program is to evaluate propellant tank ullage pressure requirements imposed by the need to accelerate propellants rapidly during the engine start sequence. These requirements can influence the system design for a given engine as well as the suitability of a given system for use with different engines. During the vehicle design phase, the SOPSA program is used to establish feed system weight variations as a function of nominal line diameter and component and line configurations. The weight data are used in conjunction with pertinent cost data to establish optimum feed system designs.
Document ID
19730019026
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 2, 2013
Publication Date
June 30, 1973
Subject Category
Space Vehicles
Report/Patent Number
LMSC-A991396-VOL-5A-2
NASA-CR-133954
Report Number: LMSC-A991396-VOL-5A-2
Report Number: NASA-CR-133954
Accession Number
73N27758
Funding Number(s)
CONTRACT_GRANT: NAS9-11330
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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