Orbital proof tests of 2 reactor auxiliary power units, Snap 10A and Snap 2, are scheduled for 1964 and 1966; their orbital operation will be observed for at least 90 days, while they perform as functional elements of fully integrated vehicle systems; safety and reliability aspects, radiological safety precautions and procedures, and other measures to be taken before launchings; reactor startup will be accomplished on fourth orbit by ground command; control and monitoring, during period from startup command through attainment of full power; radiation testing for program.


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    Title :

    Orbital testing of snap systems


    Additional title:

    Astronautics Aerospace Eng


    Contributors:


    Publication date :

    1963


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :