General Electric F404

{{Short description|Turbofan aircraft engine family}}

{{Infobox aircraft begin

|name= F404 / F412

|image= File:GE F404 engine.jpg

|caption= An F404 turbofan being tested on board an aircraft carrier

}}{{Infobox aircraft engine

|type= Turbofan

|national origin = United States

|manufacturer= General Electric

|first run= 1978

|major applications= Boeing–Saab T-7 Red Hawk
HAL Tejas Mk 1/1A
KAI T-50 Golden Eagle
Lockheed F-117 Nighthawk
McDonnell Douglas F/A-18 Hornet
Northrop F-20 Tigershark
TAI Hurjet

|number built =

|developed from = General Electric YJ101

|variants with their own articles = Volvo RM12

|developed into = General Electric F414
General Electric GE36
General Electric LM1600

}}

The General Electric F404 and F412 are a family of afterburning turbofan engines in the {{convert|10500|-|19000|lbf|kN|abbr=on|lk=on}} class (static thrust). The series is produced by GE Aerospace. Partners include Volvo Aero, which builds the RM12 variant. The F404 was developed into the larger F414 turbofan, as well as the experimental GE36 civil propfan.

Design and development

=F404=

GE developed the F404 for the F/A-18 Hornet, shortly after losing the competition for the F-15 Eagle's engine to Pratt & Whitney, and losing the Lightweight Fighter (LWF) competition to the Pratt & Whitney F100 powered YF-16. For the F/A-18, GE based the F404 on the YJ101 engine they had developed for the Northrop YF-17, enlarging the bypass ratio from 0.20 to 0.34 to enable higher fuel efficiency. The engine consists of a three-staged fan, seven axial stage compressor arrangement, single stage low and high pressure turbines, an augmentor, and produces maximum thrust of 16,000 lbf (71.2 kN) in the original F404-GE-400 model. The engine was designed with a higher priority on reliability than performance. Cost was the main goal in the design of the engine.Spick, Mike ed, Great Book of Modern Warplanes, pp. 274–278. MBI, 2000. {{ISBN|0-7603-0893-4}}.

GE also analyzed "throttle profiles" and found that pilots were changing throttle settings far more often than engineers previously expected, putting undue stress on the engines. GE also sought with the F404 a design that would avoid compressor stalls and other engine failures, and would respond quickly to control inputs; a common complaint of pilots converting from propeller planes to jets was that early turbojets were not responsive to changes in thrust input. GE executives Frederick A. Larson and Paul Setts also set the goal that the new engine would be smaller than the F-4's GE J79, but provide at least as much thrust, and cost half as much as the P&W F100 engine for the F-16.{{cite book |author=Kelly, Orr |title=Hornet: the inside story of the F/A-18 |location=Novato |publisher=Presidio Press |year=1990 |isbn=0-89141-344-8}}

Due to a fan designed to smooth airflow before it enters the compressor, the F404 has high resistance to compressor stalls, even at high angles of attack. It requires less than two shop visits per 1,000 flight hours and averages 6,500 hours between in-flight events. It also demonstrates high responsiveness to control inputs, spooling from idle to full afterburner in 4 seconds. The engine contains an in-flight engine condition monitoring system (IECMS) that monitors for critical malfunctions and keeps track of parts lifetimes.Jenkins 2000, p. 144.

GE developed the F110 for the Air Force as an alternative to the Pratt & Whitney F100 for use on the F-16 and F-15 based on the F101 and used F404 technology.{{Cite web |url=http://www.geae.com/engines/military/f110/spotlight_lockheed.html |title=GEAE: F110 Engine |access-date=2008-02-26 |archive-date=2008-02-25 |archive-url=https://web.archive.org/web/20080225110909/http://www.geae.com/engines/military/f110/spotlight_lockheed.html |url-status=dead }} The F110 was derived from the F101 via the F101DFE, though some elements of the F404 such as the design of the fan, albeit enlarged, were incorporated, per the F110 page and other sources. GE developed the F404-GE-402 in response to a Swiss requirement for more power in its F/A-18 version; it produces a maximum of 17,700 lbf (78.7 kN) of thrust with afterburner. The new engine version was used on Kuwaiti Hornets, later U.S. C and D Hornets, and subsequent Hornets.Jenkins 2000, pp. 62–63, 93, 97. The KAI T-50 Golden Eagle uses a single General Electric F404-GE-102 turbofan engine with Full Authority Digital Engine Control (FADEC) system; the engine is similar to the F404-402, but with additional redundancies built in for single-engine operations. The aircraft has a maximum speed of Mach 1.5.

Almost 4,000 F404 engines power the F/A-18 Hornets in service worldwide. The F404 engine family had totaled over 12 million flight hours by 2010.[http://www.geae.com/aboutgeae/presscenter/military/military_20100719.html "Proven Experience, Program Upgrades Spark GE F110 and F404/414 Popularity"]. {{webarchive|url=https://web.archive.org/web/20100929062201/http://geae.com/aboutgeae/presscenter/military/military_20100719.html |date=2010-09-29 }}. GE Aviation, July 19, 2010.

= F404-GE-IN20 =

For the HAL Tejas, GE developed an uprated F404-IN20, which is the highest thrust variant in F404 family, and which produces a maximum of 19,000 lbf (85 kN) of thrust with afterburner.{{cite web |title=F404 |url=https://www.geaviation.com/sites/default/files/datasheet-F404-Family.pdf |website=GE Aviation |publisher=General Electric |access-date=19 January 2022}} It incorporates latest hot section materials and technologies as well as a FADEC system for reliable power and performance.{{Cite web |title=Hindustan Aeronautics Ltd. Orders 99 F404s for Tejas Light Combat Aircraft {{!}} GE Aerospace News |url=https://www.geaerospace.com/news/press-releases/defense-engines/hindustan-aeronautics-ltd-orders-99-f404s-tejas-light-combat |access-date=2024-08-31 |website=www.geaerospace.com}} General Electric had been collaborating with Aeronautical Development Agency (ADA) for the Tejas programme since 1980s while the engine variant was chosen to power the jets in 2004.{{Cite news |date=2025-03-26 |title=GE Aerospace delivers first F404-IN20 engine to HAL for Tejas Light Combat Aircraft |url=https://economictimes.indiatimes.com/news/defence/ge-aerospace-delivers-first-f404-in20-engine-to-hal-for-tejas-light-combat-aircraft/articleshow/119521925.cms?from=mdr |access-date=2025-03-26 |work=The Economic Times |issn=0013-0389}}

India bought 10 F404-F2J3 which is used on 2 technology demonstrators and 6 prototypes of the Tejas in early 2000s.{{Cite web |date=2024-04-01 |title=ADA Launches Tender for Expert Support and Overhaul of Critical GE-F404 and GE-F414 Engines |url=https://defence.in/threads/ada-launches-tender-for-expert-support-and-overhaul-of-critical-ge-f404-and-ge-f414-engines.5023/ |access-date=2024-08-31 |website=Defence.in |language=en-US}} Two deals for 17 and 24 engines for powering LSP (including Naval prototypes) and Mk 1 IOC variants of Tejas was signed in 2004 and 2007, respectively.{{Cite web |title=GE Awarded $105 Million Development Contract from India {{!}} GE Aerospace News |url=https://www.geaerospace.com/news/press-releases/defense-engines/ge-awarded-105-million-development-contract-india |access-date=2024-08-31 |website=www.geaerospace.com}}{{Cite web |title=F404-GE-IN20 Engines Ordered for India Light Combat Aircraft {{!}} GE Aerospace News |url=https://www.geaerospace.com/news/press-releases/defense-engines/f404-ge-in20-engines-ordered-india-light-combat-aircraft |access-date=2024-08-31 |website=www.geaerospace.com}} As of September 2024, 75 engines (including F2J3 and IN20 variants) have been delivered to India.{{Cite web |last= |first= |date=2023-06-22 |title=GE Aerospace to co-produce F414 engines in India for Tejas Mk2 fighter jets |url=https://www.deccanchronicle.com/nation/current-affairs/220623/ge-aerospace-to-co-produce-f414-engines-in-india-for-tejas-mk2-fighter.html |access-date=2024-09-02 |website=www.deccanchronicle.com |language=en}} Deliveries of the engines were completed between 2008 and 2016.{{Cite web |last=Singh |first=Dalip |date=2025-03-30 |title=HAL to hand over first LCA Mk-1A to IAF in first quarter of FY26 |url=https://www.thehindubusinessline.com/economy/logistics/first-lca-mk-1a-to-be-handed-over-to-iaf-in-first-quarter-of-fy26/article69392957.ece |access-date=2025-03-31 |website=BusinessLine |language=en}}

On 17 August 2021, India signed a contract with GE worth {{INRConvert|5375|c|year=2021|lk=on}} to supply 99 F404 engines and service support by 2029.{{Cite web |title=HAL signs contract worth Rs 5,375 crore for supply of engines for Tejas aircraft |url=https://www.newindianexpress.com/nation/2021/aug/17/hal-signscontract-worth-rs-5375-crorefor-supply-of-engines-for-tejas-aircraft-2346039.html |access-date=2021-08-17 |website=The New Indian Express |date=17 August 2021 }}

However, General Electric had closed down the production line of F404-IN20 engines without further prospects of orders from India and the first engine was yet to be delivered as of October 2024 leading to the subsequent delivery delays of HAL Tejas Mk1A to the Indian Air Force. First engine delivery dates were delayed to September 2024 as of then.{{Cite news |date=2024-07-12 |title=Amid delays, HAL now aiming to deliver first LCA Mark 1A by August 15; GE engine supplies to start by September |url=https://economictimes.indiatimes.com/news/defence/amid-delays-hal-now-aiming-to-deliver-first-lca-mark-1a-by-august-15-ge-engine-supplies-to-start-by-september/articleshow/111681003.cms?from=mdr#amp_tf=From%20%251$s&aoh=17207763917473&csi=1&referrer=https://www.google.com&share=https://m.economictimes.com/news/defence/amid-delays-hal-now-aiming-to-deliver-first-lca-mark-1a-by-august-15-ge-engine-supplies-to-start-by-september/articleshow/111681003.cms |access-date=2024-07-21 |work=The Economic Times |issn=0013-0389}}{{Cite web |last=Singh |first=Rahul |date=2024-07-12 |title=GE Aerospace says working with HAL to fix new Tejas LCA engine supply delay |url=https://www.hindustantimes.com/india-news/ge-aerospace-says-working-with-hal-to-fix-delay-in-supply-of-engine-for-tejas-lca-101720787506339-amp.html |access-date=2024-07-21 |website=Hindustan Times}} Following the orders a lengthy process of sorting out supply chain problems was undertaken and the production line at Boston restarted by late 2024 to enable deliveries after a stagnation of 5 years.{{Cite news |date=2024-12-25 |title=HAL to start trial of new Tejas fighter jet in January next year |url=https://www.hindustantimes.com/india-news/hal-to-start-trial-of-new-tejas-fighter-jet-in-january-next-year-101735068257239.html |access-date=2024-12-25 |work=Hindustan Times}} The first F404-GE-IN20 engine was finally delivered to India on 25 March 2025 following a delay of two years from the expected timelines.{{Cite web |date=26 March 2025 |title=Delivering for India Today and Into the Future {{!}} GE Aerospace News |url=https://www.geaerospace.com/news/articles/delivering-india-today-and-future |access-date=2025-03-26 |website=www.geaerospace.com |language=en}}{{Cite web |last=Sharma |first=Shivani |date=2025-03-26 |title=US aerospace giant delivers first of Tejas Mk1A engines, ends 2-year delay |url=https://www.indiatoday.in/india/story/us-ge-aerospace-delivers-tejas-fighter-jet-engines-hal-delay-air-force-chief-ap-singh-2699298-2025-03-26 |access-date=2025-03-26 |website=India Today |language=en}}

=F412=

GE developed the F404 into the F412-GE-400 non-afterburning turbofan for the McDonnell Douglas A-12 Avenger II. After the cancellation of the A-12, the research was directed toward an engine for the Super Hornet, which evolved into the F414.

Applications

Specifications (F404-GE-402)

{{jetspecs

|ref=General Electric{{cite web |title=F404 Engine |url=https://www.geaviation.com/sites/default/files/datasheet-F404-Family.pdf |work=General Electric}}

|type=afterburning turbofan

|length={{convert|391|cm|abbr=on|lk=on|order=flip}}

|diameter={{convert|35|in|cm|abbr=on}} overall, {{convert|28|in|cm|abbr=on}} inlet

|Inlet diameter={{convert|28|in|cm|abbr=on}}

|weight={{convert|2,282|lb|kg|abbr=on|lk=on}}

|compressor=axial, with 3 fan and 7 HP stages

|bypass=0.34:1

|combustion=annular

|turbine=1 LP and 1 HP stage

|fueltype=

|oilsystem=

|power=

|thrust=

  • {{convert|11000|lbf|kN|abbr=on|lk=on|sigfig=3}} military thrust
  • {{convert|17700|lbf|kN|abbr=on|sigfig=3}} with afterburner

|compression=26:1

|aircon=146 lb/s (66.2 kg/s)

|turbinetemp=

|fuelcon=

|specfuelcon=

  • Military thrust: {{cvt|0.81|tsfc}}
  • Full afterburner: {{cvt|1.74|tsfc}}

|power/weight=

|thrust/weight=4.8 (dry), 7.75 (afterburning)

}}

See also

References

{{Reflist}}

  • Jenkins, Dennis R. F/A-18 Hornet: A Navy Success Story. New York: McGraw-Hill, 2000. {{ISBN|0-07-134696-1}}.