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contributor authorP. R. Edwards
contributor authorF. C. Svenson
contributor authorF. O. Chandler
date accessioned2017-05-08T23:11:34Z
date available2017-05-08T23:11:34Z
date copyrightMay, 1981
date issued1981
identifier issn1087-1357
identifier otherJMSEFK-27690#137_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/94806
description abstractThe Space Shuttle Reaction Control System design requirements, regimes of operation, and physical characteristics are described to show how they influenced the subsystem design. An overall RCS description and discussion of several components including the thruster, propellant tank, AC propellant isolation valves, and burst disc pressure relief valve assembly are presented. The current status of the Forward Reaction Control System development tests at the NASA-White Sands Test Facility are discussed including test results and unique developments encountered as a part of the test program.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Development and Testing of the Space Shuttle Reaction Control System
typeJournal Paper
journal volume103
journal issue2
journal titleJournal of Manufacturing Science and Engineering
identifier doi10.1115/1.3184468
journal fristpage137
journal lastpage143
identifier eissn1528-8935
keywordsControl systems
keywordsTesting
keywordsPropellants
keywordsDesign
keywordsSands
keywordsManufacturing
keywordsTest facilities
keywordsRelief valves
keywordsValves AND Disks
treeJournal of Manufacturing Science and Engineering:;1981:;volume( 103 ):;issue: 002
contenttypeFulltext


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