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.
ROCKET ENGINE RECOVERY SYSTEM
2016-09-29
Patent
Electronic Resource
English
IPC: | B64G Raumfahrt , COSMONAUTICS |
ROCKET ENGINE, ROCKET, AND METHOD FOR STARTING ROCKET ENGINE
European Patent Office | 2015
|ROCKET ENGINE, ROCKET, AND METHOD FOR STARTING ROCKET ENGINE
European Patent Office | 2016
|Parachute type recovery system for primary rocket body recovery and liquid rocket
European Patent Office | 2020
|