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    Atmospheric Cloud Physics Laboratory Thermal Control

    Source: Journal of Manufacturing Science and Engineering:;1979:;volume( 101 ):;issue: 002::page 191
    Author:
    J. L. Moses
    ,
    G. L. Fogal
    ,
    T. R. Scollon
    DOI: 10.1115/1.3439494
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the development background and the present status of the Atmospheric Cloud Physics Laboratory (ACPL) thermal control capability. The ACPL, a Spacelab Payload, is currently in the initial flight hardware development phase for a first flight scheduled in June 1981. The ACPL is intended as a facility for conducting a wide variety of cloud microphysics experimentation under zero gravity conditions. The cloud chambers, which are key elements of the ACPL, have stringent thermal requirements. Thus the Expansion Chamber inner walls must be uniform to within ±0.1°C during both steady state and transient operation over a temperature range of +30 to −25°C. Design progression of the Expansion Chamber, from early inhouse NASA-MSFC concepts (including test results of a prototype chamber) to the thermal control concept currently under development at General Electric, is discussed.
    keyword(s): Physics , Cloud chambers , Flight , Gravity (Force) , Temperature , Hardware , Engineering prototypes , Design AND Steady state ,
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      Atmospheric Cloud Physics Laboratory Thermal Control

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/92409
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    contributor authorJ. L. Moses
    contributor authorG. L. Fogal
    contributor authorT. R. Scollon
    date accessioned2017-05-08T23:07:13Z
    date available2017-05-08T23:07:13Z
    date copyrightMay, 1979
    date issued1979
    identifier issn1087-1357
    identifier otherJMSEFK-27677#191_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/92409
    description abstractThis paper presents the development background and the present status of the Atmospheric Cloud Physics Laboratory (ACPL) thermal control capability. The ACPL, a Spacelab Payload, is currently in the initial flight hardware development phase for a first flight scheduled in June 1981. The ACPL is intended as a facility for conducting a wide variety of cloud microphysics experimentation under zero gravity conditions. The cloud chambers, which are key elements of the ACPL, have stringent thermal requirements. Thus the Expansion Chamber inner walls must be uniform to within ±0.1°C during both steady state and transient operation over a temperature range of +30 to −25°C. Design progression of the Expansion Chamber, from early inhouse NASA-MSFC concepts (including test results of a prototype chamber) to the thermal control concept currently under development at General Electric, is discussed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAtmospheric Cloud Physics Laboratory Thermal Control
    typeJournal Paper
    journal volume101
    journal issue2
    journal titleJournal of Manufacturing Science and Engineering
    identifier doi10.1115/1.3439494
    journal fristpage191
    journal lastpage196
    identifier eissn1528-8935
    keywordsPhysics
    keywordsCloud chambers
    keywordsFlight
    keywordsGravity (Force)
    keywordsTemperature
    keywordsHardware
    keywordsEngineering prototypes
    keywordsDesign AND Steady state
    treeJournal of Manufacturing Science and Engineering:;1979:;volume( 101 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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