Energy requirements for 3-man orbit-to-orbit Earth-Mars round trip mission; capabilities of high thrust and micro-thrust systems for accomplishing mission; medium thrust nuclear electric rocket satisfying mission requirements; basic concept of thermionic nuclear magnetogas-dynamic system (TIN-MGD); vehicle configuration; nuclear and solar flare shielding; analysis shows that medium thrust vehicle could complete Earth-Mars round trip in 1 yr with payload fraction of 0.345. (See also abstract in SAE -- J v 69 n 7 July 1961 p 64-7)


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    Titel :

    Advantages of medium thrust nuclear-electric rocket


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Halle, Jr., R.W. (Autor:in) / Gronich, S. (Autor:in)

    Kongress:

    SAE Meeting ; 1961 Nuclear



    Erscheinungsdatum :

    1961


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Advantages of medium thrust nuclear-electric rocket

    Halle, Jr., R.W. / Gronich, S. | Engineering Index Backfile | 1961


    Advantages of a Medium Thrust Nuclear-Electric Rocket

    Hallet, R. W. / Gronich, S. | SAE Technical Papers | 1961


    Nuclear rocket thrust optimization using dynamic programming

    George, R.E. | Engineering Index Backfile | 1963



    Rocket Thrust Neutralizer

    G. Fountain | NTIS | 1965