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  2. 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 ...

  3. Williams J400 - Wikipedia

    en.wikipedia.org/wiki/Williams_J400

    The Williams International J400 is a small turbojet engine developed by Williams Research to power target drones. ... the WR2 which yields 125 lbs. of thrust, and the ...

  4. Workhorse SureFly - Wikipedia

    en.wikipedia.org/wiki/Workhorse_SureFly

    Each propeller blade is driven directly by an independent electric motor and flight control is achieved by varying the RPM of each blade to achieve thrust vectoring and prevailing torque changes across the vehicle, similar to smaller multirotor unmanned aerial vehicles. It was later upgraded with a 200-kW generator, a 550 lb (250 kg) payload ...

  5. 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 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 ...

  6. Pivotal BlackFly - Wikipedia

    en.wikipedia.org/wiki/Pivotal_BlackFly

    The aircraft weighs 313 lb (142 kg) empty and can carry a pilot and baggage totaling 250 lb (113 kg). It can accommodate a pilot of up to 6.5 ft (1.98 m) in height. A ballistic parachute comes equipped with the aircraft for use by the aviator in emergency situations. [1] [6] [10] The aircraft is not a tiltwing or tiltrotor design. Instead, the ...

  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. Composite Engineering BQM-167 Skeeter - Wikipedia

    en.wikipedia.org/wiki/Composite_Engineering_BQM...

    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]

  9. Teledyne CAE J69 - Wikipedia

    en.wikipedia.org/wiki/Teledyne_CAE_J69

    The Teledyne CAE J69 was a small turbojet engine originally produced by Continental Aviation and Engineering (CAE) under license from Turbomeca.The J69 was a development of the Turbomeca Marboré II.

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