This recovery system is used mainly for the recovery of liquid propellant rocket engines, so that they can be reused once or more times, in first stages (one-and-a-half) boosters. The technological goal of this invention is improved reliability of recovery systems. This goal is achieved by the rocket engine recovery system representing of a capsule comprised of a protective bottom and a lateral cover; the capsule includes a parachute bay and a landing gear bay; the capsule is attached to the engine thrust frame; at least one stabilizing parachute; at least one main parachute; at least one landing set of landing gear; the bay with the landing gear is located in the protective bottom of the capsule; the parachute release, the landing gear inflation, and the soft landing engines ignition are initiated, using simplest automatic devices.


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    Titel :

    ROCKET ENGINE RECOVERY SYSTEM



    Erscheinungsdatum :

    29.09.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS




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