FIELD: reusable hybrid aerospace transport.
SUBSTANCE: inventions group relates to the field of reusable hybrid aerospace transport with vertical take-off and landing, using a hybrid power plant, with two types of jet engines: a liquid-propellant rocket engine (LPRE) and a detonation-burning rocket-air-jet engine (RAJE) for launching spaceplanes to low reference orbit using atmospheric oxygen. The reusable hybrid launch vehicle (HLV) can be used to launch the upper stages of spacecraft into the Earth's orbit, as a reusable returnable first stage of the launch vehicle with vertical take-off and landing, and is a multifunctional hybrid reusable aircraft that combines the properties of a multicopter, aircraft, rocket and a parachute that can be transformed into a balloon, which allows for a controlled soft landing of the returned HLV. It is possible to use light fuel burnt in atmospheric air in the HLKV hybrid power plant.
EFFECT: significant reduction in the starting weight of the HLV is achieved.
4 cl, 6 dwg
