Comparison between axially and radially burning charges shows that former charge can increase missile's range more than two-fold; functional relationships between factors involved are presented in graphs; main functions are discussed mathematically; basic difference between both charges is larger amount of propellant in axially burning rocket charge.


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    Title :

    Advantages of higher combustion velocities in rocket propulsive charges


    Additional title:

    Vorteile hoeherer Abbrandgeschwindigkeiten bei Raketentreibsaetzen


    Contributors:
    Mebus, H.G. (author)

    Published in:

    Explosivstoffe ; 14 , n 4


    Publication date :

    1966


    Size :

    9 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    German


    Keywords :