The flight path of a two-staged rocket (1) is periodically calculated during flight, and the estimated impact point when a first-stage rocket body (11) or a fairing (15) is separated and discarded is periodically calculated from a second-stage rocket (13) at each passing scheduled point in the predicted flight path. As long as there is a passing scheduled point such that the estimated impact points of the first-stage rocket (11) and the fairing (15) are both within the safe area, a process is periodically performed to designate the passing scheduled point safe and nearest to ILL of the two-staged rocket (1) as the separate-and-discard point of the first-stage rocket body (11), and when the two-staged rocket (1) reaches this separate-and-discard point, the first-stage rocket body (11) or the fairing (15) is separated and discarded.


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    Title :

    CONTROL DEVICE FOR ROCKET


    Contributors:

    Publication date :

    2017-01-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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