Based on the demand of fast rendezvous and docking of manned lunar mission, it builds the mathematic model and numerical simulation to achieve the fast rendezvous and docking of manned lunar mission. It studies the necessity of spacecraft fast rendezvous and docking, researches on the present status of fast rendezvous and docking of domestic and abroad spacecraft, and obtains the realized conditions. It aims at the earth orbit and lunar orbit fast rendezvous and docking respectively, builds the spacecraft dynamical model, lunar orbit design model and constraint condition, analyzes the launch windows of the fast rendezvous and docking of earth orbit and lunar orbit by means of numerical simulation.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    On fast rendezvous and docking for manned lunar spacecraft


    Contributors:


    Publication date :

    2014-07-01


    Size :

    365508 byte





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    MANNED LUNAR LANDING VIA RENDEZVOUS

    Digesu, F. E. | NTRS | 1962


    Manned Rendezvous and Docking Technology

    Yang, Hong | Springer Verlag | 2020


    Lunar-orbit rendezvous and manned lunar landing

    Houbolt, J.C. | Engineering Index Backfile | 1962



    Trajectory and rendezvous aspects of manned lunar landings

    Enderson, L. W., Jr. / Michael, W. H., Jr. | NTRS | 1964