FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to designs of rocket systems. Unmanned aerial missile system (UAMS) with self-contained jet aircraft carrying rockets, having fuselage, carrying wing with tail unit, power plant engine (PP), onboard control system, on-board power supply, detachable anti-ship rocket (ASR), which is docked by means of separation unit with carrier and intended for surface target striking. UAMS It is equipped with at least two unmanned supersonic fighters-carriers (USFC) returned to the deck of aeronautless SC. USFC have in joint turbine winding multiple-mode three- or five-motor PP two turbojet dual-path engines (TDE) respectively with one straight-flow air-jet engine (Ramjet), mounted inside fuselage tail part in three-motor nacelle (TMN) between two afterburners TDE, or Ramjet in TMN with two Ramjet, mounted in wing gondolas at ends of inner sections of mid-superficied deltoid wing (MDW).
EFFECT: higher speed and range of flight, probability of target destruction located at long range.
4 cl, 4 dwg
