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It can carry a 159 kg (351 lb) internal payload, a 227 kg (500 lb) external payload, and has a 45 kg (99 lb)-capable weapon hardpoint on each wing. The platform is recoverable on land or at sea using a parachute system. [6] [7] In May 2017, the UTAP-22 received the official name Mako. [8] The aircraft costs between $2-$3 million. [9]
Data from Airforce Technology and Flight Global [1] [2] 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 ...
The PBS TJ150 is a Czech turbojet engine produced by PBS Velká Bíteš. The engine was developed for unmanned aerial vehicles, including target drones, as well as manned aircraft. [1] With a thrust up to 1,500N, the PBS TJ150 is the second most powerful engine in the PBS engine range. [2] The engine entered serial production in 2019. [3]
Data from General characteristics Crew: 0 Length: 18 ft 1 in (5.5 m) Wingspan: 9 ft 10 in (3.0 m) Height: 4 ft 10 in (1.47 m) Max takeoff weight: 1,464 lb (664 kg) Powerplant: 1 × Microturbo TRI 60 Turbojet Performance Maximum speed: 575 mph (925 km/h, 500 kn) Service ceiling: 40,000 ft (12,192 m) See also Aircraft of comparable role, configuration, and era Northrop BQM-74 Chukar References ...
Data from Airbus General characteristics Capacity: 100 kg (220 lb) mission payload Length: 6.2 m (20 ft 4 in) Width: 1.24 m (4 ft 1 in) Height: 2.28 m (7 ft 6 in) Max takeoff weight: 700 kg (1,543 lb) Fuel capacity: 185 L (41 imp gal; 49 US gal) Powerplant: 1 × Thielert Centurion 2.0 diesel engine, 116 kW (155 hp) Main rotor diameter: 7.2 m (23 ft 7 in) Performance Cruise speed: 220 km/h (140 ...
The BQM-74F has general configuration along the lines of the BQM-74C, but features swept wings, an empty weight of 600 lb (270 kg), an uprated engine with 300 lbf (1,300 N) of thrust, speed of up to Mach 0.93 (710 mph; 1,100 km/h), and a design lifetime of 20 flights.
This variant is an uprated model of the 60-1 engines, with thrust increased to 3.7 kN (830 lbf). [2] TRI 60-2 071: This model powers the Aerospatiale C.22 target drone, and is slight uprated to 4.0 kN (900 lbf). TRI 60-2 074: This model powers several versions of the MQM-107 Streaker drone. TRI 60-2 077: This model powers the RBS-15 anti-ship ...
The Williams International J400 is a small turbojet engine developed by Williams ... 125 lbs. of thrust, and the more powerful WR24, which yields 190-240 pounds of ...