Calculated angles, times, distances, and accelerations associated with simple one-skip maneuver to glide trajectory are presented; principal parameters are entry angle up to 6° and lift drag ratio from 1/2 to 5; results obtained by machine integrations of motion for radially symmetric earth and static ARDC atmosphere; limitations on maneuver and precision required are indicated.


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    Title :

    Dynamic analysis of simple reentry maneuver for lifting satellite


    Additional title:

    NASA -- Tech Note


    Contributors:
    Grant, F.C. (author)


    Publication date :

    1959


    Size :

    35 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :