Approach to design is based upon use of residual atmosphere to achieve satellite orientation and to provide decelerating forces which effect re-entry and allow precise control of landing point; umbrella-like steel drag brake proposed by Avco-Everett Research Laboratory consists of ribs, covering material, actuating mechanism, and capsule; principle of operation and control system philosophy; terminal velocity; drag brake potential. (See also Astronautics v 4 n 7 July 1959 p 34-5, 90, 92, 95-6)


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    Title :

    Drag brake for manned satellite recovery


    Additional title:

    Missiles Rockets


    Contributors:
    Detra, R.W. (author) / Kantrowitz, A.R. (author) / Riddell, F.R. (author) / Rose, P.H. (author)

    Published in:

    Publication date :

    1959


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Drag brake for manned satellite recovery

    Detra, R.W. / Kantrowitz, A.R. / Riddell, F.R. et al. | Engineering Index Backfile | 1959



    Manned Satellite Cabin

    S. Ta | NTIS | 1969


    Manned anti-satellite system

    Honeywell, E.E. | Engineering Index Backfile | 1963