Static aerodynamic characteristics of experimental nonlifting reentry capsule in combination with rocket booster at Mach numbers from 0.60 to 1.20


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    Title :

    Wind-Tunnel Investigation at Mach Numbers from 0.60 to 1.20 of the Static Aerodynamic Characteristics of a Model of a Possible Nonlifting Reentry Capsule in Combination with a Rocket Booster


    Contributors:

    Publication date :

    1960-09-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English