Based on estimate of probable future development of European space activities requirements for European aerospace transporter have been defined; analysis of American proposals for similar systems indicates that for expected mission (3 ton payload into near-earth orbit) systems with two parallel winged stages will represent most likely solution; for propulsion, oxygen-hydrogen rocket motors are preferred; first stage may possibly have partly air-breathing engines; aerospace transporter concept is presented.


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    Titel :

    Considerations for European reusable launch system


    Weitere Titelangaben:

    Ueberlegungen zu einem europaeischen wiederverwendbaren Traegersystem


    Beteiligte:
    Lambrecht, J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Deutsch


    Schlagwörter :


    Operational Considerations for Reusable Launch Vehicles

    Adelgren, R. G. / Ray, D. / Lashinski, P. et al. | British Library Conference Proceedings | 1997





    Some Aerodynamic and Aerothermodynamic Considerations for Reusable Launch Vehicles

    Kubota, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2004