Semianalytic method derived for calculating range of 1-stage, ballistic, rocket propelled, surface-to-surface missiles; method consists of obtaining certain analytic solutions, supposing flight in vacuum, and then correcting these solutions for effect of drag; results presented as working formulas and plots suitable for use in preliminary design studies.


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    Title :

    Ballistic missile performance


    Additional title:

    Jet Propulsion


    Contributors:
    Reece, J.W. (author) / Joseph, R.D. (author) / Schaffer, D. (author)

    Published in:

    Jet Propulsion ; 26 , n 4


    Publication date :

    1956


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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