This paper describes two complimentary experiments, the purpose of which is to measure the forces involved in the deployment in Earth orbit of a tether and its end mass. These two experiments are called TAS, (Three-axis Accelerometer System), and SEASIS, (SEDS Earth Atmospheric and Space Imaging System). The two experiments are flown as a student experiment package within a small satellite. This satellite (SEDSAT 1), which constitutes the end mass, will be deployed propulsively into a higher, permanent orbit utilizing a tethered system. These experiments are proposed to fly on a McDonnell Douglas Delta II as a secondary payload on a Global Positioning System (GPS) mission. This flight will be the third demonstration flight of the Small Expendable Deployer System (SEDS), a project managed by the NASA Marshall Space Flight Center, Huntsville, Alabama.


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    Titel :

    Complementary experiments for tether dynamics analysis


    Beteiligte:

    Kongress:

    Small-Satellite Technology and Applications ; 1991 ; Orlando,FL,United States


    Erschienen in:

    Erscheinungsdatum :

    1991-07-01





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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