Engine critical component demonstration testing continued on the main thrust chamber segment hardware. A total of 28 tests was accomplished on the 30-degree tubular-wall segment thrust chamber, and 6 tests were accomplished on the 5-inch solid-wall segment thrust chamber which was modified to shorten its combustion chamber length. Preparations continued for testing of the bearings and seals for the LF2 pumps.


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    Titel :

    Advanced Maneuvering Propulsion Technology Program


    Erscheinungsdatum :

    1969


    Format / Umfang :

    493 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch