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    Space Station Technology Readiness

    Source: Journal of Manufacturing Science and Engineering:;1984:;volume( 106 ):;issue: 004::page 260
    Author:
    R. F. Carlisle
    ,
    J. M. Romero
    DOI: 10.1115/1.3185946
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The paper discusses the meaning of “technology readiness” and how this term fits in the context of the following terms: advanced development, design maturity, risk assessment, qualification, certification, and perceived program need. The architecture of the initial module of the space station must include the provision to enable a systematic and cost-effective growth from the initial module to a space station configuration which includes two or more modules joined together in space. The paper assumes a technology readiness is required in FY 1986 to support an operational initial module of the space station in the early 1990’s. The paper defines ten disciplines/subsystems that make up the performance characteristics of a space station. Each is discussed in turn. A snapshot of the technology available in FY 1983 is used as a reference for future technology planning. A forecast of technology readiness is defined for FY 1986. The planned NASA technology and advanced development program, necessary to move the technology from the identified reference in FY 1983 to the forecast performance in FY 1986, is described including ground rules and assumptions used by NASA in the technology planning, in the use of proto-flight hardware in advanced development tests, and in the alternative techniques to be used for qualification ranging from similarity or certification through black box test or subsystem test. The paper concludes with the view that in order for the evolutionary space station to be economical, productive, and long-lived, provision for subsequent improvements and expansion in technological capability and system performance is required on the initial module. The technology options being investigated by NASA will enable the initial space station module to have provisions for reducing power costs through automated management, closing the environmental control and life support systems loops, automated subsystems, modular data network expansion, and improving human productivity. One generic technology area, automation, is pervasive in that it is an enabling technology for many of the disciplines.
    keyword(s): Space stations , Disciplines , Networks , Risk assessment , Flight , Performance characterization , Hardware AND Design ,
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      Space Station Technology Readiness

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    contributor authorR. F. Carlisle
    contributor authorJ. M. Romero
    date accessioned2017-05-08T23:18:17Z
    date available2017-05-08T23:18:17Z
    date copyrightNovember, 1984
    date issued1984
    identifier issn1087-1357
    identifier otherJMSEFK-27711#260_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/98681
    description abstractThe paper discusses the meaning of “technology readiness” and how this term fits in the context of the following terms: advanced development, design maturity, risk assessment, qualification, certification, and perceived program need. The architecture of the initial module of the space station must include the provision to enable a systematic and cost-effective growth from the initial module to a space station configuration which includes two or more modules joined together in space. The paper assumes a technology readiness is required in FY 1986 to support an operational initial module of the space station in the early 1990’s. The paper defines ten disciplines/subsystems that make up the performance characteristics of a space station. Each is discussed in turn. A snapshot of the technology available in FY 1983 is used as a reference for future technology planning. A forecast of technology readiness is defined for FY 1986. The planned NASA technology and advanced development program, necessary to move the technology from the identified reference in FY 1983 to the forecast performance in FY 1986, is described including ground rules and assumptions used by NASA in the technology planning, in the use of proto-flight hardware in advanced development tests, and in the alternative techniques to be used for qualification ranging from similarity or certification through black box test or subsystem test. The paper concludes with the view that in order for the evolutionary space station to be economical, productive, and long-lived, provision for subsequent improvements and expansion in technological capability and system performance is required on the initial module. The technology options being investigated by NASA will enable the initial space station module to have provisions for reducing power costs through automated management, closing the environmental control and life support systems loops, automated subsystems, modular data network expansion, and improving human productivity. One generic technology area, automation, is pervasive in that it is an enabling technology for many of the disciplines.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleSpace Station Technology Readiness
    typeJournal Paper
    journal volume106
    journal issue4
    journal titleJournal of Manufacturing Science and Engineering
    identifier doi10.1115/1.3185946
    journal fristpage260
    journal lastpage275
    identifier eissn1528-8935
    keywordsSpace stations
    keywordsDisciplines
    keywordsNetworks
    keywordsRisk assessment
    keywordsFlight
    keywordsPerformance characterization
    keywordsHardware AND Design
    treeJournal of Manufacturing Science and Engineering:;1984:;volume( 106 ):;issue: 004
    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