The invention discloses a high-strength light-weight detachable
fixed wing reconnaissance and
attack unmanned aerial vehicle. The unmanned aerial vehicle comprises propellers, motors, motor bases, wings, a reconnaissance holder, a front
fuselage, a rear
fuselage, a V-shaped empennage, a throwing mechanism, a front
fuselage-rear fuselage connecting mechanism used for connecting the front fuselage and the rear fuselage, and a wing-front fuselage connecting mechanism used for connecting the wings and the front fuselage. The
tail wing-rear fuselage connecting mechanism is used for connecting the V-shaped
tail wing and the rear fuselage, the motor is connected with the
propeller in the front and connected with the motor base in the rear, the two pairs of wings are symmetrically arranged on the two sides of the front fuselage through the wing-front fuselage connecting mechanism. The reconnaissance holder is arranged at the front end of the front fuselage, and is positioned behind the motor base. The reconnaissance and
attack integrated fixed-wing unmanned aerial vehicle is high in strength, low in
mass, detachable, easy to assemble, quick in
task completion and quick and accurate in
attack, and the military and civil unmanned aerial vehicle market can be quickly filled up.