Abstract A generalized rocket formula is derived from a first principles approach. The resulting expression of the thrust is applied to advanced space propulsion systems and a possible link between the asymptotic propellant velocity and the velocity at thruster exit is given. An estimation of the thrust modification due to spacecraft–plume interactions is also considered.


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    Titel :

    A generalization of the rocket formula and its application to advanced space propulsion systems


    Beteiligte:
    Nasi, L. (Autor:in) / Raimbault, J.-L. (Autor:in)

    Erschienen in:

    Acta Astronautica ; 68 , 1-2 ; 34-38


    Erscheinungsdatum :

    2010-07-26


    Format / Umfang :

    5 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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