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- Garrett_ATF3 abstract "The Garrett ATF3 (US military designation F104) is a 3-spool turbofan engine developed at the California division of Garrett AiResearch. Due to mergers it is currently supported by Honeywell Aerospace. The engine is unusual as the core flow path is twice reversed 180 deg. Aft of the fan, the axial compressor has five stages, after which the gas path progresses to the aft end of the engine. There, it is reversed 180 deg and flows through a centrifugal compressor stage, the combustors and then the turbine stages. Beyond this, the flow is then reversed 180 deg again to exit in the fan bypass duct. All engine accessories are mounted on the aft end of the engine under an engine tail-cone.The engine was first flown in the Teledyne Ryan YQM-98 Compass Cope R high altitude UAV, as the YF104-GA-100. The engine proved to have a very low infrared signature, as the hot turbine was not externally visible and the core exhaust mixed with the bypass air before exiting the engine. The pilots of U-2 high altitude chase planes reported being unable pick up the YQM-98A with either radar or IR sensors. It was later used in the Northrop Tacit Blue stealth demonstrator because of these characteristics.The most significant application of the engine was on the Dassault HU-25 Guardian, developed for the US Coast Guard. It was also used on the Dassault Falcon 20G and Dassault Falcon 200.The ATF3 was "selected by North American Rockwell for its new Series 60 Sabreliner business jet. . . . [H]owever, the ATF3 developed engineering and production problems. Delivery schedules were not met. North American Rockwell brought a $60 million suit against Garrett. . . . The suit was settled out of court for less than $5 million cash. The engine was ultimately selected for a version of the Dassault Falcon ordered by the U.S. Coast Guard for offshore surveillance".".
- Garrett_ATF3 wikiPageExternalLink portal?smap=aerospace&page=Turbofan-Products&theme=T6.
- Garrett_ATF3 wikiPageID "21107653".
- Garrett_ATF3 wikiPageRevisionID "545543607".
- Garrett_ATF3 aircon "40".
- Garrett_ATF3 combustion "Reverse flow annular type".
- Garrett_ATF3 compressor "Single Stage Low Pressure Fan, 5 stage intermediate pressure axial compressor and single stage high pressure centrifugal compressor".
- Garrett_ATF3 diameter "33.6".
- Garrett_ATF3 firstRun "1968".
- Garrett_ATF3 hasPhotoCollection Garrett_ATF3.
- Garrett_ATF3 length "102.0".
- Garrett_ATF3 lists "* List of aircraft engines".
- Garrett_ATF3 majorApplications Dassault_Falcon_20.
- Garrett_ATF3 majorApplications "Dassault Falcon 200".
- Garrett_ATF3 majorApplications "HU-25 Guardian".
- Garrett_ATF3 manufacturer Garrett_AiResearch.
- Garrett_ATF3 manufacturer "Honeywell Aerospace".
- Garrett_ATF3 nationalOrigin United_States.
- Garrett_ATF3 numberBuilt "200".
- Garrett_ATF3 thrust "5440".
- Garrett_ATF3 turbine "3".
- Garrett_ATF3 type Turbofan.
- Garrett_ATF3 type "Three shaft axial-flow turbofan".
- Garrett_ATF3 weight "1125.0".
- Garrett_ATF3 subject Category:Honeywell.
- Garrett_ATF3 subject Category:Medium-bypass_turbofan_engines.
- Garrett_ATF3 subject Category:Turbofan_engines_1960–1969.
- Garrett_ATF3 comment "The Garrett ATF3 (US military designation F104) is a 3-spool turbofan engine developed at the California division of Garrett AiResearch. Due to mergers it is currently supported by Honeywell Aerospace. The engine is unusual as the core flow path is twice reversed 180 deg. Aft of the fan, the axial compressor has five stages, after which the gas path progresses to the aft end of the engine.".
- Garrett_ATF3 label "Garrett ATF3".
- Garrett_ATF3 label "GarrettAiResearch ATF3".
- Garrett_ATF3 sameAs GarrettAiResearch_ATF3.
- Garrett_ATF3 sameAs m.05c3838.
- Garrett_ATF3 sameAs Q1494442.
- Garrett_ATF3 sameAs Q1494442.
- Garrett_ATF3 wasDerivedFrom Garrett_ATF3?oldid=545543607.
- Garrett_ATF3 isPrimaryTopicOf Garrett_ATF3.