Engineering:Oriental Titan UAV
| Oriental Titan UAV | |
|---|---|
| Role | UAV |
| National origin | China |
| Manufacturer | Beijing Oriental Titan Science and Technology JSC., Ltd. |
| Designer | 27th Research Institute of China Electronics Technologies Group Corp (CETGC) |
Oriental Titan UAVs are Chinese UAVs developed by Beijing Oriental Titan Science and Technology JSC., Ltd. (Oriental Titan, 北京东方泰坦科技股份有限公司) jointly w/ 27th Research Institute[yes|permanent dead link|dead link}}] of China Electronics Technologies Group Corp (CETGC), which sometimes is also abbreviated as CETC. Oriental Titan UAVs include both rotary and fixed wing unmanned aircraft. Oriental Titan has traditionally been a major supplier to other Chinese UAV manufacturers for imaging process system and software, and other aviation software, and now it has ventured into UAV business by developing UAVs of its own.
Agile I
Agile (Min-Jie or Minjie, 敏捷) I is an unmanned helicopter of conventional helicopter layout, and the landing gear system consists of a pair of skids. Specification:[1]
- Fuselage ength: 1.778 m
- Height: 0.711 m
- Rotor diameter: 2.146 m
- Rotor area: 0.5 m2
- Empty weight: 15 g without batteries and fuel
- Fuel: 4 l
- Normal payload: 5 kg
- Max take-off weight: 50 kg
- Max speed: 70 km/h
- Cruise speed: 60 km/h
- Rate of climb: 5 m/s
- Range: 80 km/h
- Endurance: 80 min
- Ceiling: 3.5 km
Agile II
Agile II UAV is an unmanned helicopter with conventional helicopter layout. The fuselage of Agile II is slimmer than that of Agile I, and the skids of Agile II is higher than that of Agile I, allowing Agile II to carry payload with greater height.[2]
Titan I
Titan (Tai-Tan or Titan, 泰坦) I UAV is in conventional layout with high-wing configuration and fuselage mounted tail. The UAV has a tricycle landing gear system and propulsion is provided by a two-blade propeller driven by a tractor engine mounted in the nose.[1]
Titan II
Titan II UAV is in conventional layout with high-wing configuration and fuselage mounted tail. The UAV has a tricycle landing gear system and propulsion is provided by a two-blade propeller driven by a tractor engine mounted in the nose.[1]
Titan III
Titan III UAV is a twin engine Chinese UAV developed Titan with a twin-boom layout. What is unusual about Titan III UAV is that the two engines are not mounted on the booms for the typical twin boom configuration, but instead, both engines are mounted on the fuselage, a tractor engine in the nose, and a pusher engine at the end. Both engines are equipped with two-blade propeller. This layout of Titan III is identical to that of three other Chinese UAVs: UAV Sci-Tech Telemetry IV, Hunter and ZWYX YX-3.[1]
Petrel
Petrel (Hai-Yan or Haiyan, 海燕) UAV is a fixed-wing handheld micro air vehicle of modular design that can be assembled and disassembled by hand without tools for rapidly deployment. The MAV is in conventional layout and consists of seven modules and is powered by a propeller driven by a tractor engine mounted in the nose. Specification:[2]
- Max speed: 50 km/h
- Cruise speed: 40 km/h
- Ceiling: 2.5 km
- Payload: 1 kg
- Endurance: 1 h
- Rate of climb: 5 m/s
- Range: 50 km
- Max take-off weight: 3.5 kg
- Max wind scale (speed) allowed for operation: 3 (5 m/s)
- Remote control radius: 10 km
- Power plant: electric
See also
- List of unmanned aerial vehicles of the People's Republic of China
References
- ↑ 1.0 1.1 1.2 1.3 "Agile II & Titan I/II/III". http://www.otitan.com/data_content.php?did=61. Retrieved 2012.
- ↑ 2.0 2.1 "Agile I & Petrel". http://www.81tech.com/sell/201211/23/sell25416.html. Retrieved 2012.
 |
