This article offers a summary of past efforts in the development of Nuclear Thermal Propulsion systems for space transportation. First, the generic principle of thermal propulsion is outlined: a propellant is directly heated by a power source prior to being expanded which creates a thrusting force on the rocket. This enables deriving a motivation for the use of Nuclear Thermal Propulsion (NTP) relying on nuclear power sources.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Review of Nuclear Thermal Propulsion Systems




    Erscheinungsdatum :

    2015




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch



    Klassifikation :

    BKL:    55.50 Luftfahrzeugtechnik / 55.60 Raumfahrttechnik / 55.60 / 55.50



    Review of Nuclear Thermal Propulsion Systems

    Gabrielli, Roland Antonius / Herdrich, Georg | Elsevier | 2015


    Nuclear thermal propulsion systems

    Buden, David | SLUB | 2011


    Nuclear-Thermal-Rocket Propulsion Systems

    Bruno, Claudio | AIAA | 2008


    Nuclear Thermal Rocket Propulsion Systems

    Lawrence, T.J. | Online Contents | 2007


    Nuclear Thermal Rocket Propulsion Systems

    Lawrence, T. J. / International Astronautical Federation | British Library Conference Proceedings | 2007