A rail accelerator was chosen for study as an electromagnetic space propulsion device because of its simplicity and existing technology base. The results of a mission feasibility study using a large rail accelerator for direct launch of ton-size payloads from the Earth's surface to space, and the results of initial tests with a small, laboratory rail accelerator are presented. The laboratory rail accelerator has a bore of 3 by 3 mm and has accelerated 60 mg projectiles to velocities of 300 to 1000 m/s. Rail materials of Cu, W, and Mo were tested for efficiency and erosion rate.


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    Titel :

    Rail accelerator research at Lewis Research Center


    Beteiligte:
    Kerslake, W. R. (Autor:in) / Cybyk, B. Z. (Autor:in)

    Kongress:

    Intern. Electric Propulsion Conf ; 1982 ; New Orleans


    Erscheinungsdatum :

    01.01.1982


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Rail Accelerator Research at Lewis Research Center

    W. R. Kerslake / B. Z. Cybyk | NTIS | 1982


    Rail accelerator research at Lewis Research Center

    Kerslake, W. R. / Cybyk, B. Z. | NTRS | 1982


    Rail accelerator research at Lewis Research Center

    KERSLAKE, W. / CYBYK, B. | AIAA | 1982


    Lewis Research Center program

    Soltis, D. G. | NTRS | 1977