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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 Workhorse. General characteristics Crew: 1 Capacity: 1 occupants or cargo Empty weight: 1,850 lb (839 kg) Max takeoff weight: 2,400 lb (1,089 kg) Fuel capacity: 4 x 3kWh Lithium Battery Packs for 5 min emergencies Powerplant: 1 × dual generators Fuel Piston Engine, 200 hp (150 kW) 8 × electric fixed pitch propeller Performance Maximum speed: 86 mph (139 km/h, 75 kn) Range: 70 mi ...
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 ...
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 TJ100 engine entered service in 2003, [1] and is the most popular of PBS's turbojet engines as more than 1,000 engines have been sold to 40 countries worldwide. [2] The engine has been developed for unmanned aerial vehicles , including target drones , remote carriers, unmanned combat aerial systems , light experimental jet aircraft , and ...
The engine has been developed for unmanned aerial vehicles, including target drones, remote carriers, unmanned combat systems and disposable applications with weight ranging from 330-551 lb (150-250 kg). [1] [2] The PBS TJ80-120 has the best thrust-to-weight ratio among gas turbine engines with thrust more than 1,150 N. [3] With a thrust 269 ...
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]
The Interceptor-SR shares design features of its predecessor, but is smaller and lighter weighing 1.5 kg with a 30–40 cm (12–16 in) wingspan, which the company is working to reduce to 18 cm (7.1 in) through foldable open propellers. Both designs can be directed to abort an engagement and return to its launch site to be reused.
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