NDLI: Shuttle cryogenic supply system optimization study. volume 5a-2: users manual for space shuttle orbit injection system analysis (sopsa)

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Shuttle cryogenic supply system optimization study. volume 5a-2: users manual for space shuttle orbit injection system analysis (sopsa)

Content Provider	NASA Technical Reports Server (NTRS)
Copyright Year	1973
Description	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.
File Size	4506014
Page Count	103
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19730019026
Archival Resource Key	ark:/13960/t6g20rm2m
Language	English
Publisher Date	1973-06-30
Access Restriction	Open
Subject Keyword	Space Vehicles Fuel Systems Numerical Analysis Spacecraft Components Systems Engineering Space Shuttle Orbiters Propulsion System Configurations Propellant Transfer Computer Programs Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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