FIELD: space equipment.
SUBSTANCE: group of inventions relates to space engineering, and more specifically to hybrid aerospace vehicles with vertical take-off and landing. Suborbital rocket-propelled aircraft, which combines properties of multi-copter, aircraft and missile, comprises hybrid power unit (HPU). HPU comprises control system, electric accumulator, fuel tanks and three turboprops. There is an additional compressed air supply system. Output nozzle of pendulum-gate device of reactive detonation combustion contains MHD generator.
EFFECT: enabling the application scope expansion.
4 cl, 4 dwg
Authors
Dates
2020-01-14—Published
2019-05-16—Filed