Conventional reference sensors are impractical at altitudes and velocities of planned X-15 flight path; inertial reference system used, which includes transistorized integrator amplifier with gain of 1/4 million is described.


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    Title :

    Guidance systems in manned space flight


    Additional title:

    Electronics


    Contributors:
    Cap, S.T. (author) / White, N.P. (author)

    Published in:

    Electronics ; 32 , n 33


    Publication date :

    1959


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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