The cruise and take-off thrust requirements of nuclear supersonic airplanes designed for Mach numbers of 1.5, 2, 2.5 and 3 are presented. The requirements are expressed as a function of power plant plus crew shield weight and flight altitude. The total weight of the nuclear propulsion system was varied from 140,000 pounds to 340,000 pounds and the flight altitude from 20,000 to 80,000 feet. In addition the thrust requirements of a nuclear version of the B-70 are given as a function of total nuclear propulsion system weight and flight Mach number.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Thrust Requirements for Supersonic Airplanes


    Beteiligte:
    P. G. Thome (Autor:in) / H. E. Nicoll (Autor:in)

    Erscheinungsdatum :

    1960


    Format / Umfang :

    46 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Thrust recovery in airplanes

    ENDRES STEVEN P | Europäisches Patentamt | 2018

    Freier Zugriff

    THRUST RECOVERY IN AIRPLANES

    ENDRES STEVEN P | Europäisches Patentamt | 2018

    Freier Zugriff

    Propulsion of supersonic airplanes

    Wittenberg, H. | Engineering Index Backfile | 1962


    THRUST RECOVERY IN AIRPLANES

    ENDRES STEVEN P | Europäisches Patentamt | 2016

    Freier Zugriff

    Optimal cruise trajectories for supersonic airplanes

    Teren, Fred / Daniele, Carl J. | TIBKAT | 1972