Economic feasibility of all-rocket approach to reusable launch system is investigated considering following types -- all-expendable launch vehicle, Titan IIIC; second version for recovery of payloads includes reusable reentry vehicle, TIIIC-RV; new recoverable launch system, Partial Astrorocket -- stage 1 is recovered and reused; second version for recovery of payloads includes reusable re-entry vehicle, PAR-RV; new fully recoverable launch system, Astrorocket; both stages are recovered and stage 2 has inherent capability for payload recovery; it is shown that economic feasibility of reusable launch systems is influenced strongly by need for payload recovery.


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    Titel :

    Economic justification of reusable rocket vehicles


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Spieth, C.W. (Autor:in)

    Kongress:

    SAE Meeting ; 1965 Recovery



    Erscheinungsdatum :

    1965


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    The Economic Justification of Reusable Rocket Vehicles

    Spieth, C. W. | SAE Technical Papers | 1965



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