Basic problems of liquid fuel rocket motor; choice of fuel; table gives main characteristics of several common propellant combinations at combustion chamber pressure of 20 atmos.


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    Title :

    Rockets for aircraft propulsion


    Additional title:

    Aeroplane


    Contributors:
    Allen, S. (author)

    Published in:

    Aeroplane ; 81 , n 2107


    Publication date :

    1951


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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