The aerodynamic data for the launch configuration, including separation of the three elements and abort situations are given. Presented in tabular form are the results for pitching moments, side force, right hand elevon and wing panel loads, rolling moments, and vertical tail loads.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Operational Aerodynamic Data Book. Volume 2. Launch Vehicle Aerodynamic Data, Part 2


    Publication date :

    1985


    Size :

    711 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English