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.


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    Title :

    Commonwealth Spaceflight Symposium


    Subtitle :

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



    Publication date :

    1959-10-01


    Size :

    1 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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