It is shown, that minimum drive impulse needed for transition is obtained by applying it in moment of contact with braking ellipse.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Transition of spacecraft, subject to deceleration in planet atmosphere, into orbit of artificial planet


    Additional title:

    Perekhod kosmicheskogo apparata, tormozyashchegosya v atmosfere planety, na orbitu iskustvennogo sputnika


    Contributors:
    Il'In, V.A. (author)

    Published in:

    Publication date :

    1963


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    Russian


    Keywords :



    The Outer Planet Mariner Spacecraft

    Draper, R. F. / Purdy, W. I. / Cunningham, G. | NTRS | 1975


    Spacecraft Transfer from Interplanetary to Low Near Planet Orbit by Use of Aerobraking in Venus Atmosphere

    Eismont, N. / Ledkov, A. / Nazirov, R. et al. | British Library Conference Proceedings | 2012


    Communicating with outer-planet spacecraft

    Couvillon, L. A., Jr. / Eyraud, J. P. / Kermode, A. W. et al. | NTRS | 1970