This report presents the results of an advanced di-silicide coated columbium radiation-cooled engine. The engine was designed for a nominal vacuum thrust level of 500 lbs at 20 psia, and was tested for a total duration of 218 seconds at chamber pressure between 15 psia and 20 psia. The objective of this program was to test the di-silicide, Columbium combination for durability at simulated altitude. (Author)


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    Title :

    Columbium Radiation Cooled Engine Evaluation at Simulated Altitude


    Contributors:

    Publication date :

    1965


    Size :

    36 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Coated Columbium for Gas Turbine Engine Application

    Bradley, E. F. / Hauser, H. A. / Holloway, J. F. | SAE Technical Papers | 1971


    Engine testing at simulated altitude conditions

    ROBERTS, J. / GUIDONE, J. / MANCUSO, B. et al. | AIAA | 1993


    Welding thermocouples to columbium

    Demonbrun, F. R. / Goudie, L. A. / Huguley, J. C. | NTRS | 1978


    Simulated altitude testing in USAF engine test facility

    Ferrell, J. / Harvey, R.W. | Engineering Index Backfile | 1956


    COLUMBIUM SHEET AND STRIP

    SAE Technical Papers | 1960