Installation characteristics for a Variable Stream Control Engine (VSCE) were studied for three advanced supersonic airplane designs. Sensitivity of the VSCE concept to change in technology projections was evaluated in terms of impact on overall installed performance. Based on these sensitivity results, critical technology requirements were reviewed, resulting in the reaffirmation of the following requirements: low-noise nozzle system; a high performance, low emissions duct burner and main burner; hot section technology; variable geometry components; and propulsion integration features, including an integrated electronic control system.


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    Title :

    Advanced supersonic propulsion study, phase 4


    Contributors:

    Publication date :

    1977-09-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Advanced Supersonic Propulsion Study, Phase 3

    R. A. Howlett / J. Johnson / J. Sabatella et al. | NTIS | 1976


    Advanced supersonic propulsion study, phase 3

    Howlett, R. A. / Johnson, J. / Sabatella, J. et al. | NTRS | 1976


    Advanced supersonic propulsion study

    Sabatella, J. A. | NTRS | 1974


    Advanced Supersonic Propulsion Study

    J. A. Sabatella | NTIS | 1974