Some of the conditions and methods of control and guidance for a nuclear-electric spacecraft are discussed in general terms. The type of spacecraft considered is propelled by an ion motor. The broad aspects of the flight trajectory peculiar to this type of propulsion are examined. Some equipment limitations are reviewed.


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    Title :

    Control and Guidance of Electrically Propelled Spacecraft


    Contributors:

    Publication date :

    1961-09-15


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English