The invention belongs to the field of aircrafts and discloses a low-temperature invisible multi-
nozzle aircraft. The aircraft comprises an aircraft main body, a power
system, a
control system, a bottom
nozzle, a vertical
nozzle, a horizontal nozzle, a pitching nozzle, a
tail nozzle, a
gas pipeline, a nozzle valve and a cooling and pressurizing device; the cooling and pressurizing device is locatedin the middle of the aircraft body and used for sucking, compressing and cooling part of air entering an air inlet in the front end of the power
system, storing the air and supplying the air to all the nozzles so as to change the flight attitude of the aircraft; the stored air is further supplied to the
tail nozzle and is mixed with high-temperature, high-pressure and high-speed gas flow generated by the power
system to form low-temperature, high-pressure and high-speed gas flow to be sprayed out backwards, so that pushing force is provided for the forward high-speed flight of the aircraft. Air
crash caused by the faults of flaps, ailerons, elevators and rudders can be avoided, meanwhile, heat
radiation is reduced, and the problem that existing various jet aircrafts are difficult to hidedue to high-temperature
radiation is solved.