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GZRSI GY

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GZRSI UAVs are Chinese UAVs developed by Guangzhou Guangzhou Remote Sensing Information Technology Co., Ltd. (GZRSI, 广州遥感信息科技有限公司). As of 2013, a total of four have been publicized.

Contents

GY-E1

GY-E1 UAV is an electrically powered micro air vehicle (MAV) of twin-boom layout with inverted v-tail. Proplusion is provided by two-blade propeller driven by a pusher engine installed at the rear end of the fuselage. Specification:

  • Length: 1.2 m
  • Wingspan: 2 m
  • Wing area: 0.5 m2
  • Height: 0.6 m
  • Empty weight: 2 kg
  • Payload: 1 kg
  • Max takeoff weight: 6 kg
  • Max speed: 100 km/h
  • Cruise speed: 70 km/h
  • Ceiling: 4.5 km
  • Rate of climb: 5 m/s
  • g overload: 2 g
  • Range: 30 km
  • Endurance: 30 min
  • Max wind scale (speed) allowed for operation: 4 (5 m/s)
  • Remote control radius: 50 km

    • GY-X1

    GY-X1 is a multirotor UAV developed by GZRSI with a total of eight two-blade rotors arranged in four pairs. For each pair, one rotor is mounted above the arm, while the other below the arm.

    GY-Y1

    GY-Y1 is a gasoline-powered UAV with conventional layout. Propulsion is provided by a two-blade propeller driven by a tractor engine mounted in the nose, and the landing gear system consists of a pair of skids. Specification:

  • Length: 1.8 m
  • Wingspan: 2.6 m
  • Wing area: 0.9 m2
  • Height: 0.5 m
  • Empty weight: 14 kg
  • Payload: 4.5 kg
  • Max takeoff weight: 20 kg
  • Max speed: 140 km/h
  • Cruise speed: 110 km/h
  • Ceiling: 4.5 km
  • Rate of climb: 8 m/s
  • g overload: 3 g
  • Range: 100 km
  • Endurance: 1.5 h
  • Max wind scale (speed) allowed for operation: 5 (8 m/s)
  • Remote control radius: 50 km

    • GY-Y2

    GY-Y1 is a gasoline-powered UAV with conventional layout, and it is a large cousin of GY-Y1. As with its smaller cousin GY-Y1, propulsion for GY-Y2 is provided by a two-blade propeller driven by a tractor engine mounted in the nose, and the landing gear system consists of a pair of skids. Specification:

  • Length: 2 m
  • Wingspan: 3 m
  • Wing area: 1.2 m2
  • Height: 0.55 m
  • Empty weight: 20 kg
  • Payload: 8 kg
  • Max takeoff weight: 34 kg
  • Max speed: 140 km/h
  • Cruise speed: 110 km/h
  • Ceiling: 4.5 km
  • Rate of climb: 10 m/s
  • g overload: 3 g
  • Range: 300 km
  • Endurance: 4 h
  • Max wind scale (speed) allowed for operation: 5 (8 m/s)
  • Remote control radius: 50 km

    • References

    GZRSI GY Wikipedia
    (Text) CC BY-SA


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