Soar Dragon High-Altitude Long Endurance Reconnaissance UAV
SKU: MD-P00141·UAV Platforms·حسب الطلب
نظرة عامة
Manufacture： Guizhou Aircraft Industry Corporation The Soar Dragon uav, designed by Chengdu Aircraft Corporation and constructed by Guizhou Aircraft Industry Corporation for service with the People's Liberation Army Air Force, was originally displayed as a model at the Zhuhai Air Show in 2006. Optimised for long-endurance missions at high altitude, the aircraft features an unusual tandem, joined wing platform. Except for the wing and the configuration of vertical stabilizers, the Soar Dragon is similar in appearance and mission to the Northrop Grumman RQ-4 Global Hawk operated by the United States Air Force. Large by the standards of UAVs, the Soar Dragon's joined wing allows for a more rigid, less flexible wing than other configurations, with benefits said to include an increased lift-to-drag ratio and less complex flight controls than a HALE UAV with a conventional wing would require. The aircraft is powered by a Guizhou WP-13 turbojet engine, a copy of the Soviet Tumansky R-13; it is anticipated that a newer, improved engine, will be installed in production aircraft. The air intake for the engine is mounted atop the fuselage, with the engine itself mounted in the rear of the aircraft. Soar Dragon Drone Specifications Length: 14.33 m (47 ft 0 in) Wingspan: 24.86 m (81 ft 7 in) Height: 5.41 m (17 ft 9 in) Powerplant: 1 Guizhou WP-13 turbojet, 43.1 kN (9,700 lbf) thrust Cruise speed: 750 km/h (466 mph, 405 kn) Range: 7,000 km (4,300 mi, 3,800 nmi) Combat range: 2,000 km (1,200 mi, 1,100 nmi) Service ceiling: 18,000 m (59,000 ft) New Xianglong Soaring Dragon drones may also have application as tactical jammers. 29 Jul 2019 China s New Soar Dragon Spy Drone Tailed a US Cruiser in Taiwan Strait 22:00 29.07.2019 China has deployed EA-03 Soar Dragon long-range reconnaissance drones at the Shigatse Peace Airport in the Tibet Autonomous Region Oct 7, 2017
المواصفات التقنية
Specifications. المواصفات الرئيسية: Manufacture Guizhou Aircraft Industry Corporation، Crew None، Length 14.33 m (47 ft 0 in)، Wingspan 24.86 m (81 ft 7 in)، Height 5.41 m (17 ft 9 in)، Powerplant 1 Guizhou WP-13 turbojet, 43.1 kN (9,700 lbf) thrust، Cruise speed 750 km/h (466 mph, 405 kn)، Range 7,000 km (4,300 mi, 3,800 nmi)، Combat range 2,000 km (1,200 mi, 1,100 nmi)، Endurance 10 hours، Service ceiling 18,000 m (59,000 ft)، Thrust/weight 5.8.
المواصفات التقنية — 1 groups
المواصفات الرئيسية: Manufacture Guizhou Aircraft Industry Corporation، Crew None، Length 14.33 m (47 ft 0 in)، Wingspan 24.86 m (81 ft 7 in)، Height 5.41 m (17 ft 9 in)، Powerplant 1 Guizhou WP-13 turbojet, 43.1 kN (9,700 lbf) thrust، Cruise speed 750 km/h (466 mph, 405 kn)، Range 7,000 km (4,300 mi, 3,800 nmi)، Combat range 2,000 km (1,200 mi, 1,100 nmi)، Endurance 10 hours، Service ceiling 18,000 m (59,000 ft)، Thrust/weight 5.8.
المواصفات الفنية
Specifications
- Manufacture
- Guizhou Aircraft Industry Corporation
- Crew
- None
- Length
- 14.33 m (47 ft 0 in)
- Wingspan
- 24.86 m (81 ft 7 in)
- Height
- 5.41 m (17 ft 9 in)
- Powerplant
- 1 Guizhou WP-13 turbojet, 43.1 kN (9,700 lbf) thrust
- Cruise speed
- 750 km/h (466 mph, 405 kn)
- Range
- 7,000 km (4,300 mi, 3,800 nmi)
- Combat range
- 2,000 km (1,200 mi, 1,100 nmi)
- Endurance
- 10 hours
- Service ceiling
- 18,000 m (59,000 ft)
- Thrust/weight
- 5.8