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Data from Airforce Technology and Flight Global General characteristics Capacity: 65.7 kg Length: 13 ft 9 in (4.2 m) Wingspan: 11 ft 5 in (3.47 m) Width: 1 ft 10 in (0.57 m) Height: 1 ft 8 in (0.52 m) Gross weight: 1,499 lb (680 kg) Powerplant: 1 × Williams F107 turbofan engine, 700 lbf (3.1 kN) thrust Performance Maximum speed: Mach 0.6 Range: 350 mi (560 km, 300 nmi) See also List of X ...
Netra can be launched from a small clearing, and it can fly up to a distance of 2.5 km from its take-off point. The operational altitude of the UAV is 200 m. With an on-board wireless transmitter, it can carry out surveillance in an area of 1.5 km Line of Sight (LOS) at the height of 300 m, for 30 minutes on a single battery charge.
In this test flight, the UAV flew for 30 minutes at an altitude of 910 m (3,000 ft). The test was conducted in Hosur. [21] The Indian army was impressed with Rustom-1 and will use it as a MALE UAV. Rustom-1 made its 5th successful flight on morning of 12 November 2011, flying for 25 minutes at 700 m (2,300 ft) AGL at a speed 190 km/h (100 kn).
The Boeing X-50A Dragonfly, formerly known as the Canard Rotor/Wing Demonstrator, was a VTOL rotor wing experimental unmanned aerial vehicle that was developed by Boeing and DARPA to demonstrate the principle that a helicopter's rotor could be stopped in flight and act as a fixed wing, enabling it to transition between fixed-wing and rotary ...
The Wing Loong II UAV MALE is an enlarged version of the Wing Loong I with a longer body and wider wing span. It has a slender fuselage, V-tail , and ventral fin. The aircraft features retractable landing gear, including two main wheels under the fuselage and one single wheel under the nose.
Data from Heron/Shoval/Eitan General characteristics Capacity: 250 kg (551 lb) Length: 8.5 m (27 ft 11 in) Wingspan: 16.6 m (54 ft 6 in) Airfoil: IAI SA-21 Max takeoff weight: 1,150 kg (2,535 lb) Powerplant: 1 × Rotax 916 4-cylinder air and water cooled horizontally-opposed piston engine, 160 kW (210 hp) Propellers: 3-bladed pusher propeller Performance Maximum speed: 207 km/h (129 mph, 112 ...
A Medium-Altitude Long-Endurance (MALE) UAV, the Gray Eagle has an increased wingspan compared to the original MQ-1 Predator and is powered by a Thielert Centurion 1.7 Heavy Fuel Engine (HFE). [24] This is a Diesel piston engine that burns jet fuel, giving the aircraft better performance at high altitudes.
WJ-1 The armed version of Pterodactyl I, which is a weapon platform without the reconnaissance/targeting pod under the chin. The designation WJ stands for Wu-Zhuang Wu-Ren-Ji (武装无人机), meaning armed UAV. WJ-1 UAV made its public debut in November 2014 at the 10th Zhuhai Airshow along with its cousin GJ-1. [48] GJ-1