A description of the structure and uses of the Long Duration Exposure Facility (LDEF) is given. The LDEF was designed to provide a large number of economical opportunities for science and technology experiments that require modest electrical power and data processing while in space and which benefit from postflight laboratory investigations with the retrieved experiment hardware. Like the Shuttle, the LDEF is reusable, and repeat missions are planned, each with a new complement of experiments. The LDEF is essentially a free-flying cylindrical structure. The experiments on LDEF are totally self-contained in trays mounted on the exterior of the structure. LDEF can accommodate 86 experiment trays, 72 around the circumference and 14 on the two ends. The LDEF is delivered to Earth orbit by the Shuttle. In orbit, the Shuttle remote manipulator system removes the LDEF from the Shuttle payload bay and places it in a gravity-gradient-stabilized attitude. After an extended period in orbit, which is set by experiment requirements, the LDEF is retrieved on a subsequent Shuttle flight.


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    Titel :

    Introduction to Long-Duration Exposure Facility


    Beteiligte:
    Kinard, W. H. (Autor:in)


    Erscheinungsdatum :

    01.02.1984


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Long Duration Exposure Facility surface temperatures

    HUGHES, P. C. / TENNYSON, R. C. | AIAA | 1992


    Long Duration Exposure Facility (LDEF) results

    Kinard, William H. / O'Neal, Robert L. | NTRS | 1991


    Long Duration Exposure Facility (LDEF) results

    KINARD, WILLIAM / O'NEAL, ROBERT | AIAA | 1991