dual-mode chemical rocket engine, dual-mode propulsion system, spacecraft, use of a bipropellant combination, and method for pulse generation

摘要

1/1 overview “dual-mode chemical rocket engine, dual-mode propulsion system, space vehicle, use of a bipropellant combination, and method for impulse generation” The invention generally relates to dual-mode bipropellant chemical rocket propulsion systems for use in aerospace applications for 1) orbit lifting, maintenance and maneuvering. orbit, altitude control and spacecraft deorbital, and / or 2) propellant sedimentation, scroll and altitude control of missiles, launchers and space planes. The present invention also relates to a dual mode chemical rocket engine for use in such systems. The engine uses low-risk storable liquid propellants and can be operated in either single propellant or bipropellant mode. The monopropellants used are a fuel-rich low-risk liquid monopropellant and hydrogen peroxide, respectively.