A wide variety of potentially useful and effective airbreathing aircraft have been postulated to operate at speeds in excess of Mach 3.0 by NASA and the USAF. These systems include hydrogen-fueled transports of interest for very long ranges and airbreathing launch vehicles which are aircraft-type first stage candidates for future space shuttle systems. Other high speed airbreathing systems for possible future military applications include advanced reconnaissance and figher/interceptor type aircraft and strategic systems. This paper presents (1) a chronology of Air Force technical activity on future propulsion concepts, (2) a status report on NASA research on scramjet technology for future systems which may require speeds above Mach 5, and (3) a description of a research vehicle by which advanced propulsion technology and other technologies related to high speed can be demonstrated.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Propulsion Concepts for High Speed Aircraft


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    Aerospace Engineering and Manufacturing Meeting ; 1975



    Erscheinungsdatum :

    1975-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Propulsion concepts for high speed aircraft

    Stull, F. D. / Jones, R. A. / Zima, W. P. | NTRS | 1975



    Propulsion system concepts for silent aircraft

    Manneville, Alexis, 1978- | DSpace@MIT | 2004

    Freier Zugriff

    HIGH-SPEED HYBRID PROPULSION FOR AIRCRAFT

    NISSEN JEFFREY PAUL / SCHANK TROY CYRIL | Europäisches Patentamt | 2020

    Freier Zugriff

    HIGH-SPEED HYBRID PROPULSION FOR AIRCRAFT

    SCHANK TROY CYRIL / NISSEN JEFFREY PAUL | Europäisches Patentamt | 2021

    Freier Zugriff