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  2. PBS TJ150 - Wikipedia

    en.wikipedia.org/wiki/PBS_TJ150

    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]

  3. Airbus Helicopters VSR700 - Wikipedia

    en.wikipedia.org/wiki/Airbus_Helicopters_VSR700

    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 ...

  4. CASC Rainbow - Wikipedia

    en.wikipedia.org/wiki/CASC_Rainbow

    A more recent engine variant, with a 300kW piston engine from Anhui Hangrui Co., will increase the service ceiling to 12 km and the endurance life to 120 hours. [23] Armaments: AR-1 missile, AR-2 missile (20 kg, 5 kg armour-piercing warhead, inertial guidance system with terminal semi-active laser (SAL) seeker, maximum range 8 km) [18]

  5. TAPAS-BH-201 - Wikipedia

    en.wikipedia.org/wiki/TAPAS-BH-201

    The Tactical Airborne Platform for Aerial Surveillance Beyond Horizon-201 [2] or TAPAS BH-201(lit. ' Heat ') (formerly referred to as Rustom-II until 2016 [3]) is a medium-altitude long-endurance (MALE) [4] unmanned aerial vehicle (UAV) being developed in India by Aeronautical Development Establishment (ADE) on the lines of General Atomics MQ-1 Predator.

  6. CAIG Wing Loong II - Wikipedia

    en.wikipedia.org/wiki/CAIG_Wing_Loong_II

    Yes, 1000 kg 3300 kg Turboprop 220 km/h 60 hours for recon / 30 hours with 8 AR-1 missiles GJ-1 (Wing Loong I) Yes, 200 kg 1100 kg Piston 280 km/h 20 hours GJ-2 (Wing Loong II) Yes, 480 kg 4200 kg Turboprop 370 km/h 32 hours / 20 hours at max speed Wing Loong III Yes, 2300 kg 6200 kg Turboprop - 40 hours WZ-10 (Wing Loong-10) Yes, 400 kg 3200 kg

  7. Northrop BQM-74 Chukar - Wikipedia

    en.wikipedia.org/wiki/Northrop_BQM-74_Chukar

    The BQM-74C can be air launched as well as ground launched. The original engine was the Williams WR24-7A AKA J400-WR-402, with 180 lbf (800 N) of thrust, but in 1986 production was upgraded to the J400-WR-403 with 240 lbf (1,100 N) of thrust. The BQM-74C is stressed for maneuvers of up to 6g. More than 1,600 BQM-74Cs have been built.

  8. Teledyne CAE J402 - Wikipedia

    en.wikipedia.org/wiki/Teledyne_CAE_J402

    The Teledyne CAE J402 is an American small turbojet engine. Several variants have been developed to power unmanned air vehicles such as missiles and target drones. Developed in the 1970s for the Harpoon anti-ship missile, the J402 was the first jet engine to be designed as a "wooden round", meaning that the engine had to be able to sit for long periods without maintenance or inspection and ...

  9. Microturbo TRI 60 - Wikipedia

    en.wikipedia.org/wiki/Microturbo_TRI_60

    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 Aérospatiale 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 ...

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