PD-1

Unmanned Aerial System

One stop UAS solution for civil and military applications

THE MOST FLEXIBLE UAV PLATFORM ON THE MARKET

PD–1 UAV is multipurpose modular fixed–wing UAV with a wide range of options and payloads to fit any mission and operational environment. It is a combat–proven solution  since 2016 and previously tested for 2 years. During this time, the PD–1 UAS has proved its performance capabilities, anti–jamming features, and overall effectiveness while being able to operate in harsh environment.

The PD–1 drone is packed with high–end technology, featuring a reliable flight controller, an AES–256–encrypted digital data link, anti–jamming features, inertial navigation unit, navigation lights and much more other features to make drone operations safe and easy.


TECHNICAL SPECIFICATIONS

Flight controller is compliant with DO178 & DO254 standards.

  • MTOW 40 kg
  • Max payload 10 kg with full fuel tank
  • Wingspan 4 m
  • Length 2.5 m
  • Propulsion system 4–stroke
  • Takeoff method; Runway / catapult / VTOL
  • Endurance 10+ hours
  • Service ceiling 3000 m
  • Cruise speed 25 m/s
  • Stall speed 16 m/s
  • Takeoff run 100 m (fully loaded)


PD–1 UAV Specifications

  • Maximum takeoff weight 40 kg
  • Empty weight 22 kg (with undrainable fuel)
  • Payload weight 10 kg
  • Flight time with 4–storke engine 10+ hours
  • Flight time with EFl upgrade Up to 15 hours
  • Practical ceiling 3000 m
  • Speed range 70–140 km/h
  • Cruise speed 95 km/h
  • Stall speed 50 km/h
  • Fuel A–95 mixed with oil
  • Deployment time 15 min
  • Launch Runway, catapult, VTOL
  • Recovery Runway, parachute, VTOL
  • Navigation GNSS, inertial navigation unit

Dimensions

  • Full length 2540 mm
  • Height 990 mm
  • Chassis track 670 mm
  • Chassis wheelbase 880 mm
  • Main wheel size 150x31 mm
  • Nose wheel size 127x31 mm
  • Wing area 1/17 m2
  • Wingspan 4000 mm
  • Mean wing chord 392 mm
  • Tip wing chord 300 mm
  • Root wing chord 420 mm
  • Aileron area 2x0.06 m
  • Flaps area 2x0.055 m2
  • Fuselage max width 266 mm
  • Fuselage max height 284 mm
  • Full projection area of V–tail on horizontal plane 0.278 m2
  • Full projection area of V–tail on vertical plane 0,123 m2