The concept of reusing spacecraft and launch vehicles is currently exemplified by the Space Shuttle Orbiter and the two recoverable and reusable solid rocket boosters (SRBs) which are part of its launch system. It is shown that it is possible to recover launch systems weighing as much as one million pounds at reasonable impact velocities using a hybrid parachute-retrorocket recovery system. The new Kevlar materials, which have a much higher strength-to-weight ratio than nylon materials, make it possible to recover a one-million-pound booster for a reasonable weight penalty. The selected input parameters to the parachute weight equation result in an accurate estimation of the current Space Shuttle solid rocket booster parachute recovery system.


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    Titel :

    Feasibility of recovering a one million-pound booster


    Beteiligte:
    Toni, R. A. (Autor:in) / Eckstrom, C. V. (Autor:in)

    Kongress:

    International Meeting and Technical Display on Global Technology 2000 ; 1980 ; Baltimore, MD


    Erscheinungsdatum :

    01.05.1980


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Feasibility of recovering a one million-pound booster

    TONI, R. / ECKSTROM, C. | AIAA | 1980



    Hoverports -- Million-pound afterthought

    Sarony, P. | Engineering Index Backfile | 1967