Main phases of 10-yr European space program (1961-1971) comprise development of: launching vehicle of size and payload capacity comparable to largest operational in United States; launching vehicle, utilizing higher energy propellants in upper stages to increase payload capacity; launching vehicle, capable of placing 10, 000 kg in close orbit, based on high energy-propellant stages, with 500,000 kg total thrust cluster of liquid hydrogen/lox engines in first stage; applications.


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    Title :

    Ten year programme of space technology


    Additional title:

    Spaceflight


    Contributors:

    Published in:

    Spaceflight ; 3 , n 6


    Publication date :

    1961


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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