Abstract The paper considers the ballistic design of spacecraft (SC) transfer to the neighborhood of the L2 point and subsequent entry of the SC into the halo orbit. Trajectory calculations of one-impulse Earth-halo orbit transfers with and without using a lunar gravitational maneuver are presented. For the calculation of one-impulse trajectories of Earth-halo-orbit transfers, an algorithm for constructing initial approximations is applied. These approximations are constructed by calculating and analyzing the isolines as a function of two variables. This function is represented by the pericenter height of the outgoing orbit over the Earth’s surface. The arguments of the function are special parameters that characterize the halo orbit. The mentioned algorithm allows one to obtain halo orbits with specified geometrical characteristics both in the ecliptic plane, and in the plane orthogonal to it. The estimates of the characteristic velocity expenses for maintaining SC in the selected halo orbit are obtained. The described technique was used to search for working orbits of the Spectr-RG and Millimetron spacecraft. Examples of orbits obtained are presented.


    Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Ballistic design of transfer trajectories from artificial-satellite earth orbit to halo orbit in the neighborhood of the L2 point of the Sun-Earth system


    Contributors:

    Published in:

    Publication date :

    2014




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.93 Weltraumforschung / 39.00 Astronomie: Allgemeines / 55.60 Raumfahrttechnik
    Local classification TIB:    770/3520/8000




    Transfer Trajectories From Low Earth Orbit to a Large L~1-Centered Class I Halo Orbit in the Sun-Earth Circular Problem

    Kechichian, J. A. / American Astronautical Society | British Library Conference Proceedings | 2000


    Design method of earth-moon system L1 point translation point orbit-earth low-energy transfer orbit

    WANG MINGMING / LIU WEI / LUO JIANJUN et al. | European Patent Office | 2024

    Free access

    Sun-Earth L1 Region Halo-to-Halo Orbit and Halo-to-Lissajous Orbit Transfers

    Roberts, C. E. / German Space Operations Center / European Space Operations Centre | British Library Conference Proceedings | 2004