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Shuttle cryogenic supply system optimization studyTechnical information on different cryogenic supply systems is presented for selecting representative designs. Parametric data and sensitivity studies, and an evaluation of related technology status are included. An integrated mathematical model for hardware program support was developed. The life support system, power generation, and propellant supply are considered. The major study conclusions are the following: Optimum integrated systems tend towards maximizing liquid storage. Vacuum jacketing of tanks is a major effect on integrated systems. Subcritical storage advantages over supercritical storage decrease as the quantity of propellant or reactant decreases. Shuttle duty cycles are not severe. The operational mode has a significant effect on reliability. Components are available for most subsystem applications. Subsystems and components require a minimum amount of technology development.
Document ID
19720005128
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
August 6, 2013
Publication Date
September 30, 1971
Subject Category
Propellants
Report/Patent Number
LMSC-A995668
NASA-CR-124626
Report Number: LMSC-A995668
Report Number: NASA-CR-124626
Accession Number
72N12777
Funding Number(s)
CONTRACT_GRANT: NAS9-11330
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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