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.


    Access

    Download


    Export, share and cite



    Title :

    ROCKET ENGINE RECOVERY SYSTEM



    Publication date :

    2016-09-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    ROCKET ENGINE, ROCKET, AND METHOD FOR STARTING ROCKET ENGINE

    KAWAMATA YOSHIHIRO / OBASE KIMIHITO | European Patent Office | 2015

    Free access

    ROCKET ENGINE, ROCKET, AND METHOD FOR STARTING ROCKET ENGINE

    KAWAMATA YOSHIHIRO / OBASE KIMIHITO | European Patent Office | 2016

    Free access

    Rocket recovery system

    YANG WEIJIE / LI DINGSHI / XU XUELEI et al. | European Patent Office | 2024

    Free access

    Parachute type recovery system for primary rocket body recovery and liquid rocket

    YANG RUIKANG / CHE LINA / HAN JIANYE et al. | European Patent Office | 2020

    Free access

    Rocket sublevel recovery system

    WANG YINGCHENG / SHI XIAONING / WANG JINGJING et al. | European Patent Office | 2024

    Free access