Abstract We review analytical formulae for low-thrust orbital transfers from a circular initial orbit to a circular target orbit and to escape, using constant thrust applied in the same direction as the velocity vector, or in the opposite direction. The formulae give approximations for the maneuver time, final mass fraction, and evolution of the semimajor axis. For comparison, the associated results for high-thrust Hohmann and Oberth transfers are summarized. A simple computer program employing the aforementioned relationships is a useful tool for analysis of planar planetary and interplanetary space missions. This implementation yields fast and reasonably accurate approximations to trajectory performance boundaries. Consequently, the approach can provide trajectory analysis for each spacecraft configuration during the conceptual space mission design phase. As an example, a mission from Low-Earth Orbit (LEO) to Jupiter’s moon Europa is analyzed.


    Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Planar High-Thrust and Low-Thrust Orbital Transfers from Earth to Europa




    Publication date :

    2004




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    55.60 Raumfahrttechnik
    Local classification TIB:    770/7040




    Planar High-Thrust and Low-Thrust Orbital Transfers from Earth to Europa

    Seywald, Hans / Roithmayr, Carlos M. / Mazanek, Daniel D. et al. | Springer Verlag | 2004


    Planar High-Thrust and Low-Thrust Orbital Transfers From Earth to Europa (AAS 03-146)

    Seywald, H. / Roithmayr, C. M. / Mazanek, D. D. et al. | British Library Conference Proceedings | 2003


    Finite thrust orbital transfers

    Mazzini, Leonardo | Online Contents | 2014


    Finite thrust orbital transfers

    Mazzini, Leonardo | Elsevier | 2014