Wind tunnel stability tests of space shuttle model at subsonic to hypersonic speeds


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Space shuttle: Effect of orbiter incidence angle on the aerodynamic characteristics of the Boeing S-IC booster/ GAC G-11 orbiter launch configuration, M equal .6 to 4.96


    Contributors:

    Publication date :

    1971-08-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :