A new trajectory design approach for lift-control reentry flight vehicle based on cruising design concept is proposed in this paper. The cruising parameter could be aerodynamic overload, dynamic pressure, or aeroheating rate at stagnation point. For a high speed reentry flight vehicle, based on this trajectory design approach, it could firstly cruise at an appropriate aeroheating rate, then at an appropriate aerodynamic overload, and finally at an appropriate dynamic pressure. As an example, the entry trajectories designed for a certain lift-control reentry vehicle based on the new approach are presented in this paper, too.


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    Title :

    A New Reentry Trajectory Design Approach for Lift-control Flight Vehicle Based on Cruising Design Concept


    Contributors:


    Publication date :

    2018-08-01


    Size :

    408989 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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