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F404 / F412
An F404 turbofan being tested on board an aircraft carrier
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
Developed from	General Electric YJ101
Variants	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 10,500–19,000 lbf (47–85 kN) 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.

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.

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.

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. 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. 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.

GE F404-IN20

For 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. It incorporates latest hot section materials and technologies as well as FADEC system for reliable power and performance. India bought 10 F404-F2J3 which is used on 2 Technology Demonstrators and 6 prototypes of Tejas in early 2000s. 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. As of September 2024, 75 engines (including F2J3 and IN20 variants) have been delivered to India.

On 17 August 2021, India signed a contract with GE worth ₹5,375 crore (equivalent to ₹60 billion or US$720 million in 2023) to supply 99 F404 engines and service support by 2029. However, the first engine of the deal signed in 2021 is yet to be delivered as of October 2024 which has led to the delay of delivery of HAL Tejas Mk1A aircraft to the Indian Air Force. Earlier reports suggested that engine delivery was expected to be commenced from September 2024 at the rate of 1-2 per month.

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

F404

• Boeing Phantom Ray
• Boeing X-45C
• Boeing–Saab T-7 Red Hawk
• FMA SAIA 90 (as designed, not built)
• Dassault Rafale A (prototype only)
• Grumman A-6F Intruder II
• Grumman X-29
• HAL Tejas Mk 1/1A
• Lockheed F-117 Nighthawk
• KAI T-50 Golden Eagle
• McDonnell Douglas F/A-18 Hornet (A-D)
• Northrop F-20 Tigershark
• Scaled Composites Model 400
• Rockwell-MBB X-31
• ST Aerospace A-4SU Super Skyhawk
• TAI Hürjet

F412

• McDonnell Douglas A-12 Avenger II (as designed, not built)

Specifications (F404-GE-402)

Data from General Electric

General characteristics

• Type: afterburning turbofan
• Length: 154 in (391 cm)
• Diameter: 35 in (89 cm) overall, 28 in (71 cm) inlet
• Dry weight: 2,282 lb (1,035 kg)

Components

• Compressor: axial, with 3 fan and 7 HP stages
• Combustors: annular
• Turbine: 1 LP and 1 HP stage

Performance

• Maximum thrust:
  
  • 11,000 lbf (48.9 kN) military thrust
  • 17,700 lbf (78.7 kN) with afterburner
• Overall pressure ratio: 26:1
• Bypass ratio: 0.34:1
• Air mass flow: 146 lb/s (66.2 kg/s)
• Specific fuel consumption:
  
  • Military thrust: 0.81 lb/(lbf⋅h) (23 g/(kN⋅s))
  • Full afterburner: 1.74 lb/(lbf⋅h) (49 g/(kN⋅s))
• Thrust-to-weight ratio: 4.8 (dry), 7.75 (afterburning)

See also

Related development

• General Electric YJ101
• General Electric F414
• General Electric F110
• Volvo RM12

Comparable engines

• GTRE GTX-35VS Kaveri
• Guizhou WS-13
• Klimov RD-33
• Snecma M88
• Turbo-Union RB199

Related lists

• List of aircraft engines

References

1. Spick, Mike ed, Great Book of Modern Warplanes, pp. 274–278. MBI, 2000. ISBN 0-7603-0893-4.
2. Kelly, Orr (1990). Hornet: the inside story of the F/A-18. Novato: Presidio Press. ISBN 0-89141-344-8.
3. Jenkins 2000, p. 144.
4. "GEAE: F110 Engine". Archived from the original on 2008-02-25. Retrieved 2008-02-26.
5. ^ Jenkins 2000, pp. 62–63, 93, 97.
6. "Proven Experience, Program Upgrades Spark GE F110 and F404/414 Popularity". Archived 2010-09-29 at the Wayback Machine. GE Aviation, July 19, 2010.
7. "F404" (PDF). GE Aviation. General Electric. Retrieved 19 January 2022.
8. ^ "F404-GE-IN20 Engines Ordered for India Light Combat Aircraft | GE Aerospace News". www.geaerospace.com. Retrieved 2024-08-31.
9. ^ "Hindustan Aeronautics Ltd. Orders 99 F404s for Tejas Light Combat Aircraft | GE Aerospace News". www.geaerospace.com. Retrieved 2024-08-31.
10. "ADA Launches Tender for Expert Support and Overhaul of Critical GE-F404 and GE-F414 Engines". Defence.in. 2024-04-01. Retrieved 2024-08-31.
11. "GE Awarded $105 Million Development Contract from India | GE Aerospace News". www.geaerospace.com. Retrieved 2024-08-31.
12. "GE Aerospace to co-produce F414 engines in India for Tejas Mk2 fighter jets". www.deccanchronicle.com. 2023-06-22. Retrieved 2024-09-02.
13. "HAL signs contract worth Rs 5,375 crore for supply of engines for Tejas aircraft". The New Indian Express. 17 August 2021. Retrieved 2021-08-17.
14. "Amid delays, HAL now aiming to deliver first LCA Mark 1A by August 15; GE engine supplies to start by September". The Economic Times. 2024-07-12. ISSN 0013-0389. Retrieved 2024-07-21.
15. Singh, Rahul (2024-07-12). "GE Aerospace says working with HAL to fix new Tejas LCA engine supply delay". Hindustan Times. Retrieved 2024-07-21.
16. "F404 Engine" (PDF). General Electric.

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

External links

• GE Aviation F404 page
• F404 page on GlobalSecurity.org

• Low-bypass turbofan engines
• General Electric aircraft engines
• 1970s turbofan engines