DP-14 Hawk American Autonomous Unmanned Helicopter
DP-14 Hawk



The DP-14 Hawk is a heavy-lift variant of the DP-6 Whisper designed for missions such as air supply to forward in operation bases. it's designed to hold up to 430 lb (195 kg) of payload in its twenty six cu ft (0.7 copper m) of cargo area or external hardpoints. It will reportedly fly for about 2.4 hours with a 430-lb payload or 4.3 hours with a 100-lb (45-kg) payload. The DP-14 will operate in crosswinds of up to forty knots (74 kmh). The air vehicle would be powered by either AN 87-hp star T62 engine or a 133-hp Microturbo eAPU rotary engine and is intended to use either JP-5 or JP-8 significant fuel. The power plant would generate 4.2 kW of power for avionics and sensors. The DP-14 Hawk uses aboard measuring system and advanced algorithms to navigate in complicated, restricted environments, as well as advanced intelligence for path coming up with, course corrections, perception, obstacle dodging and landing-site choice. These capabilities permit the air vehicle to fly intelligent, autonomous, non-line-of-sight, nap-of-the-earth missions and dynamically adapt to changes on the wing conditions and terrain, according to Dragonfly Pictures. The system employs imu and GPS for takeoff and landing and an supersonic sensing element as a measuring device to see height from the bottom throughout landing. These sensors allow landings even in brownouts or different degraded visual environments. The air vehicle is equipped with 2 side-mounted pods for over-sized things. The unmanned chopper features one ms autopilot cycling and speedy pitch correction throughout autonomous cargo offloading, that permits precision airdrops with accuracy of higher than 10 ft (3 m). It needs a landing site measurement regarding 60 ft (18 m) x 60 ft (18 m). All-terrain undercarriage supports landings on uneven ground; slopes of up to 15 degrees; and heaving ship decks. A relative positioning system permits the DP-14 to self-launch and self-recover on pitching ships with an 8-in (203-mm) circular error probable. The system is assembled, readied and launched inside half-hour.