The conceptual design configuration of a nuclear electric propulsion system (NEP) with a multimission capability for both earth orbital and electric propulsion missions is discussed. Two basic types of space reactor power system concepts are analyzed emphasizing conduction coupled and radiation coupled systems, and a radiation coupled thermoelectric panel concept is schematically represented and described in detail. A nuclear-powered 100-kWe surveillance spacecraft concept is presented and the developmental phases are given including cost estimates. In addition, a system is described that seems to have the capability to perform all the outer planet missions.


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    Title :

    Multimission nuclear electric propulsion system for outer planet exploration missions


    Contributors:

    Conference:

    International Electric Propulsion Conference ; 1981 ; Las Vegas, NV, US


    Publication date :

    1981-04-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English