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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 ...
The Century Series is a popular name for a group of US fighter aircraft representing models designated between F-100 and F-106 which went into full production. They included the first successful supersonic aircraft designs in the United States Air Force 's service, which remained in active service well into the 1970s and 1980s with the Air ...
ADC (from "Aircraft Disposal Company") [3] bought 35,000 war-surplus engines in 1920. Initially produced engines from Renault 70 hp spares. ADC Cirrus. ADC Airdisco; ADC Cirrus; ADC Nimbus, development of Siddeley Puma; ADC Airsix, air-cooled version of Nimbus. Not put into use; ADC BR2 [1] ADC Viper [1] ADC Airdisco-Renault [1]
United States military aircraft engine designations; W. Water injection (engine) This page was last edited on 3 January 2014, at 02:33 (UTC). Text ...
The General Electric F110 is an afterburning turbofan jet engine produced by GE Aerospace (formerly GE Aviation). It was derived from the General Electric F101 as an alternative engine to the Pratt & Whitney F100 for powering tactical fighter aircraft, with the F-16C Fighting Falcon and F-14A+/B Tomcat being the initial platforms; the F110 would eventually power new F-15 Eagle variants as well.
The North American F-100 Super Sabre is an American supersonic jet fighter aircraft designed and produced by the aircraft manufacturer North American Aviation. The first of the Century Series of American jet fighters, it was the first United States Air Force (USAF) fighter capable of supersonic speed in level flight .
In 1910, Hall-Scott also began manufacturing aircraft engines for commercial and military aviation. [4] These engines possessed a remarkable power-to-weight ratio for the era, [citation needed] using an overhead cam, overhead valves, hemispherical combustion chamber, and extensive use of aluminum. Their various engine types shared parts and ...
The F118 is a non-afterburning derivative of the F110 specially developed for the B-2 Spirit stealth bomber. A single stage HP turbine drives the 9 stage HP compressor, while a 2-stage LP turbine drives the 3 stage fan.
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