Recommended propulsion system for 900-lb Lunar Reconnaissance Vehicle is comprised of solid rocket motor and pressurized positive expulsion liquid bi-propellant system feeding 4 radiation-cooled attitude engines in 1-lb thrust class; vernier engines provide midcourse correction on translunar trajectory, second stage impulse of retro-maneuver, and impulse for lunar orbit maneuvers; attitude control engines are used to orient vehicle to desired inertial position during translunar coast period, orient vehicle for midcourse, retro, and lunar maneuver, and impart spin rate, to vehicle prior to retro-maneuver.


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    Titel :

    Preliminary propulsion considerations for lunar orbiting reconnaissance vehicle


    Weitere Titelangaben:

    Israel J Technology


    Beteiligte:
    Cutler, M. (Autor:in)

    Erschienen in:

    Israel Journal of Technology ; 2 , n 1 ; p 201-207


    Erscheinungsdatum :

    1964


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    LUNAR LANDING PROPULSION CONSIDERATIONS

    Stehling, K. R. | NTRS | 1963




    Solid Propulsion De-Orbiting and Re-Orbiting

    Schonenborg, R.A.C. / Schoyer, H.F.R. | British Library Conference Proceedings | 2009


    Lunar Orbiting Observatory Mission

    Kaneko, Y. / Takizawa, Y. / Kawazoe, T. et al. | British Library Conference Proceedings | 1995