The performance goals of the NASP program require an aero-propulsion system with a high effective specific impulse. In order to achieve these goals, the high potential performance of air-breathing engines must be achieved over a very wide Mach number operating range. This, in turn, demands high component performance and involves many important technical issues which must be resolved. Scramjet Propulsion Technology is divided into five major areas: (1) inlets, (2) combustors, (3) nozzles, (4) component integration, and (5) test facilities. A status report covering the five areas is presented.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    NASP X-30 Propulsion technology status


    Beteiligte:


    Erscheinungsdatum :

    01.01.1992


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    NASP X-30 Propulsion Technology Status

    W. E. Powell | NTIS | 1992


    CFD propels NASP propulsion progress

    Povinelli, Louis A. / Dwoyer, Douglas L. / Green, Michael J. | NTRS | 1990


    NASP - A status report

    THOMAS, JR., JOHN / POWELL, WILLIAM | AIAA | 1992


    NASP - A status report

    Thomas, John P., Jr. / Powell, William E. | NTRS | 1992


    NASP technology transfer

    Morris, Charles | NTRS | 1992