TYW-1 Reconnaissance and Strike UAV
SKU: MD-P00146·UAV Platforms·حسب الطلب



نظرة عامة
The TYW-1 UAV, developed by Beihang University in Beijing, one of China's top institutes for science and technology, is an unmanned aircraft for reconnaissance and combat based on the BZK-005 high-altitude, long-range reconnaissance drone, which the university also developed. Unveiled on 13 November China s TYW-1 strike-capable reconnaissance UAV features four underwing pylons and is reported to have a maximum take-off weight of 1,500 kg. The TYW-1, which has a wingspan of 18 m, features the same pusher-engine, twin-boom, outward-canted stabiliser design of the BZK-005, the latter of which is believed to be in service with the People s Liberation Army (PLA). The 9.85 m-long and 2.5 m-high TYW-1, however, is reported to have a maximum take-off weight of 1,500 kg compared with the 1,250 kg of the BZK-005. According to Chinese media reports, the TYW-1 can carry a 370 kg payload, features four underwing pylons, has a ceiling of 7.5 km, an endurance of 40 hours, and can reach a top speed of 200 km/h. The UAV is also equipped with an electro-optical system that can reportedly read a licence plate 50 km away from an altitude of 5,000 m. It also features both line-of-sight and satellite navigation and control systems. The company also displayed what appeared to be a new version of the BZK-005 featuring a system mounted under the UAV s nose that could be electronic support measures (ESM), a radar, or a communication relay. n early April 2016 the BZK-005 was spotted on Woody Island in the South China Sea, and in September 2013 Japan Air Self-Defense Force F-15J aircraft intercepted a BZK-005 flying near the disputed Senkaku/Diaoyu Islands. Beihang Unmanned Aircraft System Technology is an offshoot of the Beijing University of Aeronautics and Astronautics (BUAA), which originally developed the BZK-005 together with the Harbin Aircraft Industry Group.
المواصفات التقنية
Specifications. المواصفات الرئيسية: Max Take-off Weight 500 kg، Endurance 40 h، Max Speed 200 km/h، Wingspan 18 m.
المواصفات التقنية — 1 groups
المواصفات الرئيسية: Max Take-off Weight 500 kg، Endurance 40 h، Max Speed 200 km/h، Wingspan 18 m.
المواصفات الفنية
Specifications
- Max Take-off Weight
- 500 kg
- Endurance
- 40 h
- Max Speed
- 200 km/h
- Wingspan
- 18 m