Flight data from Saturn I have established base thermal environment of eight-engine LOX/RP-1 rockets; plume radiation levels, total heating rates, and base gas temperatures have been measured on first stage of Block I and II vehicles; some heating data also were obtained for six-engine LOX/LH2, S-IV second-stage base; flight instrumentation, data reduction techniques, and evaluation problems are discussed along with correlation of flight results to long- and short-duration model tests.


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    Title :

    Summary of Saturn I base thermal environment


    Additional title:

    J Spacecraft Rockets


    Contributors:
    Payne, R.G. (author)

    Published in:

    Publication date :

    1966


    Size :

    9 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Summary of saturn i base thermal environment.

    Jones, I. P., Jr. / Payne, R. G. | NTRS | 1965




    Summary of Saturn I base thermal environment.

    Jones, I. P. / Payne, R. G. | NTRS | 1966