GZRSI GY
GZRSI GY | |
---|---|
Role | UAV |
National origin | China |
Designer | Guangzhou |
Number built | 4 |
|
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.
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:[1]
- Length: 1.2 m
- Wingspan: 2 m
- Wing area: 0.5 m2
- Height: 0.6 m
- Empty weight: 2 kg
- Payload: 1 kg
- Max take off 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.[2]
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:[3]
- 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 take off 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:[4]
- Length: 2 m
- Wingspan: 3 m
- Wing area: 1.2 m2
- Height: 0.55 m
- Empty weight: 20 kg
- Payload: 8 kg
- Max take off 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
See also
List of unmanned aerial vehicles of the People's Republic of China