System, developed to provide control at high altitudes in regions of low dynamic pressure and to operate at zero normal acceleration and in extremely low-temperature environment, consists of storage vessel, pressurization system, flow control system, and rocket units; on-off control is used with which rockets are operated at fixed thrust levels of from 20 to 40 lb; problems encountered, fabrication of system, and data pertinent to performance characteristics.


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    Title :

    Hydrogen-peroxide rocket reaction-control system for X-1b research airplane


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1959


    Size :

    28 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English





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