Application of these systems is examined for unmanned flybys and orbiter missions, and manned missions to Mercury, Mars, and Jupiter; characteristics such as power requirements and required operational lifetimes of electric systems are shown for several manned missions in which separate power plants for outbound and inbound phases are employed; use of combined electric systems could increase payloads for given initial mass in Earth orbit in case of near-planet orbiters and flybys and even reduce long trip times to more distant planets; for manned Jupiter mission, trip time of 1500 days appears to be attractive on basis of mass, power requirements, and operating times of electric power plants.


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    Title :

    Applications of combined electric, high-thrust propulsion systems


    Additional title:

    J Spacecraft Rockets


    Contributors:
    Mascy, A.C. (author) / Dugan, D.W. (author) / Pitts, S.W. (author)

    Published in:

    Publication date :

    1968


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Applications of combined electric, high-thrust propulsion systems.

    DUGAN, D. W. / MASCY, A. C. / PITTS, S. W. | AIAA | 1968


    Applications of combined electric, high-thrust propulsion systems.

    Dugan, D. W. / Mascy, A. C. / Pitts, S. W. | NTRS | 1968


    Applications of combined high-thrust, low- thrust propulsion systems

    DUGAN, D. / MASCY, A. / PITTS, S. | AIAA | 1967


    Applications of combined high-thrust, low- thrust propulsion systems.

    Dugan, D. W. / Mascy, A. C. / Pitts, S. W. | NTRS | 1967