This paper aims to suggest a new thermonuclear space propulsion and electric generator for aerospace.

    Design/methodology/approach

    Methods of thermonuclear physics are used for research.

    Findings

    The paper applies, develops and researches mini-sized Micro-AB thermonuclear reactors for space propulsion and space power systems. These small engines directly convert the high-speed charged particles produced in the thermonuclear reactor into vehicle thrust or vehicle electricity with maximum efficiency. The simplest AB-thermonuclear propulsion offered allows spaceships to reach speeds of 20,000-50,000 km/s (1/6 of light speed) for fuel ratio 0.1 and produces a huge amount of useful electric energy. The offered propulsion system permits flight to any planet of the solar system in a short time and to the nearest non-Sun stars by E-being or intellectual robots during a single human life period.

    Research limitations/implications

    Technical limitations may be apparent.

    Originality/value

    The theory of this propulsion and electric generator is developed and possibilities researched.


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    Titel :

    Simplest AB-thermonuclear space propulsion and electric generator


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    2008-01-25


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Simplest AB-thermonuclear space propulsion and electric generator

    Bolonkin, Alexander | Online Contents | 2008


    Towards Thermonuclear Rocket Propulsion

    Englert, G. W. | NTRS | 1962


    Preliminary study of thermonuclear rocket propulsion

    Roth, J.R. | Engineering Index Backfile | 1961