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GA-ASI's design is larger than the Sea Avenger and is powered by the Pratt & Whitney PW815 high-bypass turbofan, the same engine used on the Gulfstream G600. Generating 16,000 lb (7,300 kg) of thrust, it is four times more powerful than the Predator C's PW545B turbofan, [31] and the most powerful engine used by any Stingray competitor. [32]
First run 1987. Flown in twin-engine MBB BO105 for demonstration only. [2] PW206A Maximum continuous power 550 shp (410 kW) [3] for use on the MD Explorer PW206B Maximum continuous power 431 shp (321 kW), [3] for use on the Eurocopter EC135 PW206B2 Maximum continuous power 431 shp (321 kW). [3] PW206C
The General Atomics "Predator B-001", a proof-of-concept aircraft, first flew on 2 February 2001. Abraham Karem is the designer of the Predator. [8] The B-001 was powered by an AlliedSignal Garrett TPE331-10T turboprop engine with 950 shaft horsepower (710 kW).
The 715 shp TPE331-6 used in the Beech King Air B100 have a 400-hr. fuel nozzle cleaning interval, 1,800-hr. hot section inspection interval and a 5,400-hr. time between overhaul; approval is possible for 3,000-hr. HSIs and 6,000-hr. overhauls and engine reserves are cheaper than for the PT6A.
The F-16C/D Block 30/32s were the first to be built with the common engine bay, able to accept the existing F100-200/220 engine (Block 32) or the F110-100 (Block 30). A non-afterburning variant, the F100-PW-220U powers the Northrop Grumman X-47B UCAV. The -100 and -200 series engines could be upgraded to become equivalent to -220 specifications ...
External fuel tanks can add 450 lb (200 kg) of extra fuel, allowing for a 50-hour endurance. The IGE also increases internal payload capacity from 400 lb (180 kg) to 540 lb (240 kg). [13] The empty weight is 1,318 kg (2,906 lb), endurance without the external tank is 45 hours, and engine can sustain an output of 180 hp (130 kW) continuously.
In December 1980, Pratt & Whitney changed to a new naming system for its engines and the JT10D became the PW2037. The PW2000 is a dual-spool, axial air flow, annular combustion, high bypass turbofan with a dual-channel full authority digital engine control system. It was certified in 1984 as the first civilian FADEC-controlled aviation engine.
The Rotax 914 is a turbo-charged, four-stroke, four-cylinder, horizontally opposed aircraft engine with air-cooled cylinders and water-cooled cylinder heads.It is designed and built by the Austrian company BRP-Powertrain, owned by Bombardier Recreational Products (BRP), as part of its Rotax brand.
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