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 SAE -- Paper 338A for meeting Apr 4-7 1961 9 p)


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    Title :

    Advantages of medium thrust nuclear-electric rocket


    Additional title:

    SAE -- J


    Contributors:


    Publication date :

    1961


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    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