Characteristics of ballistic missile and design of nose cone primary purpose of which is to provide thermal protection for payload; factors considered in study of Missile and Space Vehicle Dept of General Electric Co selecting material to protect Atlas re-entry nose cone at ICBM ranges; flight test program and method of obtaining data with copper heat sink re-entry vehicle over range of re-entry conditions.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Nose cones -- Case for heat sink


    Additional title:

    Missiles Rockets


    Contributors:

    Published in:

    Publication date :

    1959


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Tangent-ogive nose cones

    Wing, L. D. | NTRS | 1976


    Manufacturing Ablative Nozzles and Nose Cones

    Rechin, F. J. | SAE Technical Papers | 1965


    SUPERSONIC PROJECTILE NOSE CONES WITH FLAT TIPS

    CARY ANDREW W / DORGAN ANDREW J | European Patent Office | 2016

    Free access


    Carbon skinned aluminium foam nose cones for high performance circuit vehicles

    Chirwa, E C / Latchford, J / Clavell, P | Online Contents | 2003