Details of rocket capable of carrying sounding probes and payloads of 25 and 100 lb to altitudes of 525 and 300 nautical mi, respectively; data obtained from typical flight test of system.


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    Title :

    Five-stage solid-fuel sounding-rocket system


    Additional title:

    NASA -- Memo


    Contributors:


    Publication date :

    1959


    Size :

    22 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English





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    Shaver, R.D. | Engineering Index Backfile | 1967


    The Two-Stage Sounding-Rocket Problem

    R. D. Shaver | NTIS | 1967


    The two-stage sounding rocket problem.

    SHAVER, R. D. | AIAA | 1967