The Chengdu Aircraft Industry Group (CAIG) took the wraps off its second-generation Wing Loong MALE UCAV at the Beijing Air Show from 16-19 September. Powered by a turboprop engine, the aircraft has a ...

The Wing-Loong II has a maximum flying altitude of more than 29,500 feet, a speed of about 211 miles per hour and a flight endurance of 20 hours.

In the past, Taiwanese reports have identified the BZK-005 ISR drone and TB-001 reconnaissance-strike UAV flying into Taiwan's ADIZ, while the Wing Loong-2 and Wing Loong-10 (also known as Wuzhen ...

The Wing-Loong II is a medium-altitude, long-endurance, multi-role UAS integrated with both reconnaissance and strike capabilities. ... It has a maximum take-off weight of 4.2 tonnes, ...

The Wing-Loong II is a medium-altitude, long-endurance, multi-role UAS integrated with both reconnaissance and strike capabilities. ... It has a maximum take-off weight of 4.2 tonnes, with an external ...

According to AVIC, the Wing Loong II has a maximum take-off weight of 4,200kg (9,300lb), nearly four times greater than the Wing Loong I. It also has six hard points, compared with just two for ...

Chinese airframer AVIC is displaying a mock-up of its Wing Loong II armed UAV in the static park. The Wing Loong II is an updated version of the Wing Loong I. According to AVIC, the Wing Loong II ...

Morocco's reported purchase of the Chinese Chengdu Wing Loong II drone is merely the latest example of a country diversifying its drone fleet. With the addition of these armed Chinese unmanned ...

This photograph released by Taiwan Ministry of National Defense taken from a Taiwan Air Force F-16V, shows a Chinese CAIG Wing Loong II drone near Taiwan, Monday, March 17, 2025. (Taiwan Ministry ...

China Unveils CH-9, Wing Loong-X Platforms For Naval Applications Defense Digest Get free defense news, insight and analysis from our award-winning editors delivered to your inbox daily.

Even at a high-altitude airport of 4,000 meters above sea level, the Wing-Loong 1E can take off and land normally under the maximum weight condition of the external configuration.