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    The Development and Testing of the Space Shuttle Reaction Control System

    Source: Journal of Manufacturing Science and Engineering:;1981:;volume( 103 ):;issue: 002::page 137
    Author:
    P. R. Edwards
    ,
    F. C. Svenson
    ,
    F. O. Chandler
    DOI: 10.1115/1.3184468
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The 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.
    keyword(s): Control systems , Testing , Propellants , Design , Sands , Manufacturing , Test facilities , Relief valves , Valves AND Disks ,
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      The Development and Testing of the Space Shuttle Reaction Control System

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/94806
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    • Journal of Manufacturing Science and Engineering

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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
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian