Spinning solid propellant upper stage rocket engines designed for geosynchronous satellite payloads are investigated. Factors considered include: impact of the spinning stages on the payloads; applicability to 1981-1991 NASA mission model; and cost effectiveness.


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    Title :

    STS spin-stabilized upper stage study (study 2.6). Volume 1: Executive summary


    Publication date :

    1975-09-30


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English