Effect of rocket and launcher design parameters on the maximum height obtainable in vertical flight. Comparison of costs for single- and two-stage rockets. If efficiencies of around 100,000 ft./lb. payload/lb. propellent can be realized in practice, small solid propellent rockets should prove economical for routine meterological use.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Commonwealth Spaceflight Symposium


    Untertitel :

    Summaries of Papers given at the Symposium held at Church House, Westminster, London, August 27–29, 1959



    Erscheinungsdatum :

    01.10.1959


    Format / Umfang :

    1 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    IAC IAF Human Spaceflight Symposium

    International Astronautical Federation | DataCite | 2022


    IAC IAF Human Spaceflight Symposium

    International Astronautical Federation | DataCite | 2011


    Spaceflight Versus Human Spaceflight

    Barr, S. / International Association for the Advancement of Space Safety | British Library Conference Proceedings | 2013