Lockheed YF-22
YF-22 | |
---|---|
A YF-22 during a test flight | |
Role | Stealth fighter technology demonstrator |
National origin | United States |
Manufacturer | Lockheed / Boeing / General Dynamics |
First flight | 29 September 1990 |
Status | Retired |
Primary user | United States Air Force |
Produced | 1989–1990 |
Number built | 2 |
Developed into | Lockheed Martin F-22 Raptor |
The Lockheed/Boeing/General Dynamics YF-22 is an American single-seat, twin-engine
In the 1980s, the USAF began looking for a replacement for its fighter aircraft, especially to counter the advanced
Design and development
In 1981, the U.S. Air Force developed a requirement for an Advanced Tactical Fighter (ATF) as a new air superiority fighter to replace the F-15 Eagle and F-16 Fighting Falcon. This was made more crucial by the emerging worldwide threats, including development and proliferation of Soviet MiG-29 and Su-27 "Flanker"-class fighter aircraft. It would take advantage of the new technologies in fighter design on the horizon including composite materials, lightweight alloys, advanced flight-control systems, more powerful propulsion systems and stealth technology.[1] In September 1985, the Air Force sent out technical request for proposals (RFP) to a number of aircraft manufacturing teams. The seven bids were submitted in July 1986, and two companies, Lockheed and Northrop, were selected on 31 October 1986. The two teams, Lockheed/Boeing/General Dynamics and Northrop/McDonnell Douglas, undertook a 50-month demonstration phase, culminating in the flight test of the two teams' prototypes, the YF-22 and the YF-23.[2][3][4]
The YF-22A was designed to meet USAF requirements for survivability,
The YF-22 was given the unofficial name "Lightning II" after Lockheed's World War II-era fighter, the P-38 Lightning, which persisted until the mid-1990s when the USAF officially named the aircraft "Raptor".[10] The F-35 later received the "Lightning II" name in 2006.[11]
Formally designated as the YF-22A, the first aircraft (PAV-1,
Operational history
Evaluation
During the flight test program, unlike the YF-23, weapon firings and high (60°) angle of attack (AoA, or high-alpha) flights were carried out on the YF-22.[16] Though not a requirement, the aircraft fired AIM-9 Sidewinder and AIM-120 AMRAAM missiles from internal weapon bays.[16][17] Flight testing also demonstrated that the YF-22 with its thrust vectoring nozzles achieved pitch rates more than double that of the F-16 at low-speed maneuvering. The first prototype, PAV-1 with the General Electric engines, achieved Mach 1.58 in supercruise, while PAV-2 with the Pratt & Whitney engines reached a maximum supercruise speed of Mach 1.43; maximum speed was in excess of Mach 2.0.[18][19] Flight testing continued until 28 December 1990, by which time 74 flights were completed and 91.6 airborne hours were accumulated.[4] Following flight testing, the contractor teams submitted proposals for ATF production.[20]
On 23 April 1991, the YF-22 was announced by Secretary of the Air Force Donald Rice as the winner of the ATF competition.[21] While both designs met or exceeded all performance requirements, the YF-23 was stealthier and faster, but the YF-22 was more agile.[22] It was speculated in the aviation press that the YF-22 was also seen as more adaptable to the Navy's Navalized Advanced Tactical Fighter (NATF), but the US Navy abandoned NATF by 1992.[16][23] Instead of being retired, as with the case of PAV-1, PAV-2 subsequently flew sorties following the competition – it amassed another 61.6 flying hours during 39 flights.[16] On 25 April 1992, the aircraft sustained serious damage during a landing attempt as a result of pilot-induced oscillations. It was repaired but never flew again, and instead served as a static test vehicle thereafter.[24][25] In 1991, it was anticipated that 650 production F-22s would be procured.[26]
F-22 production
As the Lockheed team won the ATF competition, it was awarded the engineering, manufacturing and development (EMD) contract, which would ultimately allow it to proceed with production of operational aircraft. The EMD called for seven single-seat F-22A and two twin-seat F-22Bs. On 9 April 1997, the first of these, Spirit of America, was rolled out. During the ceremony, the F-22 was officially named "Raptor". Due to limited funding, the first flight, which had previously been scheduled for mid-1996, occurred on 7 September 1997.
In many respects, the YF-22s were different from EMD/production F-22s. Contrary to the F-117 Nighthawk, which was initially difficult to control because of small vertical stabilizers, Lockheed over-specified the fin area on its YF-22. Therefore, the company reduced the size of those on F-22s by 20–30 percent. Lockheed recontoured the shape of the wing and stabilator trailing edges to improve aerodynamics, strength, and stealth characteristics; the wing and stabilitor sweep was reduced by 6° from 48°. The shapes of the radome and fuselage were changed to improve radar performance and aerodynamics. Finally, to improve pilot visibility, the canopy was moved forward 7 inches (178 mm), and the engine intakes were moved rearward 14 inches (356 mm).[28][29][30]
Accidents
In April 1992, the second YF-22 crashed while landing at Edwards AFB. The test pilot, Tom Morgenfeld, escaped without injury. The cause of the crash was found to be a flight control
Surviving aircraft
- YF-22A PAV-1, S/N 87-0700 –
- YF-22A PAV-2, S/N 87-0701 – Rome Laboratory, Rome, New York.[33]
Specifications (YF-22A)
Data from Baker and Aronstein (note, some specifications are estimated).[34][35]
General characteristics
- Crew: 1 (pilot)
- Length: 64 ft 6 in (19.65 m)
- Wingspan: 43 ft 0 in (13.1 m)
- Height: 17 ft 9 in (5.39 m)
- Wing area: 830 sq ft (77.1 m2)
- Empty weight: 33,000 lb (14,970 kg)
- Gross weight: 62,000 lb (28,120 kg)
- Powerplant: 2 × Pratt & Whitney YF119-PW-100 or General Electric YF120-GE-100 afterburning turbofans, 23,500 lbf (105 kN) thrust each (YF120) dry, 30,000 or 35,000 lbf (130 or 160 kN) with afterburner
Performance
- Maximum speed: Mach 2.2 (1,450 mph, 2,335 km/h) at altitude
- Supercruise: Mach 1.58 (1,040 mph, 1,680 km/h) at altitude (military power only)
- Combat range: 800 mi (1,290 km, 696 nmi)
- Service ceiling: 65,000 ft (19,800 m)
- Maximum g-load: +7.9 g
See also
Related development
- Lockheed Martin F-22 Raptor – American stealth air superiority fighter
- Lockheed Martin FB-22 – Proposed bomber aircraft for the US Air Force derived from the F-22 Raptor
- Lockheed Martin X-44 MANTA – Conceptual aircraft design by Lockheed Martin
Aircraft of comparable role, configuration, and era
- Northrop YF-23 – Prototype fighter aircraft for the US Air Force Advanced Tactical Fighter program
Related lists
References
Notes
- ^ a b "Fact sheet: Lockheed-Boeing-General Dynamics YF-22". U.S. Air Force. 11 February 2009. Archived from the original on 19 January 2012. Retrieved 18 June 2011.
- ^ Miller 2005, pp. 19–20.
- ^ Jenkins and Landis 2008, pp. 233–234.
- ^ a b Williams 2002, pp. 5–6.
- ^ Flight International 1986, p. 10.
- ^ a b c d Jenkins and Landis 2008, p. 235.
- ^ Flight International 1990, p. 4.
- ^ Flight International 1990, p. 46.
- ^ "YF-23 fact sheet". National Museum of the U.S. Air Force. Archived from the original on 16 July 2011. Retrieved 24 June 2011.
- ^ "Military Aircraft Names". Aerospaceweb.org. Archived from the original on 12 October 2009. Retrieved 26 September 2010.
- ^ ""Lockheed Martin Joint Strike Fighter Officially Named 'Lightning II'" (Press release). Official Joint Strike Fighter program office. 7 July 2006. Archived from the original on 15 July 2006. Retrieved 23 June 2011.
- ^ Williams 2002, p. 5.
- ^ a b c Flight International 1990, p. 6.
- ^ Bailey 1990, p. 34.
- ^ Goodall 1992, p. 99.
- ^ a b c d Williams 2002, p. 6.
- ^ "YF-23 would undergo subtle changes if it wins competition". Defense Daily, 14 January 1991
- ^ Jenkins and Landis 2008, p. 236.
- ^ Goodall 1992, pp. 102–103.
- ^ Miller 2005, pp. 38–39.
- ^ Jenkins and Landis 2008, p. 234.
- ^ Goodall 1992, p. 110.
- ^ Miller 2005, p. 76.
- ^ a b William 2002, pp. 6–7.
- ^ Warwick 1992, p. 12.
- ^ Pearlstein, Steven; Gellman, Barton (24 April 1991). "Lockheed Wins Huge Jet Contract; Air Force Plans to Buy 650 Stealth Planes At $100 million Each". The Washington Post.
- ^ "F-22A Raptor goes operational". U.S. Air Force. 15 December 2005. Archived from the original on 23 July 2012. Retrieved 24 June 2011.
- ^ William 2002, p. 5.
- ^ Pace 1999, pp. 12–13.
- ^ "YF-22/F-22A comparison diagram". GlobalSecurity.org. Archived from the original on 23 June 2011. Retrieved 24 June 2011.
- ^ Harris, Jeffery and Black, G.T. "F-22 control law development and flying qualities." AIAA Paper 96-3379 (A96-35101), p. 156.
- ^ "YF-22 Raptor/87-700". aerialvisuals.ca. Retrieved 18 June 2021.
- ^ "YF-22 Raptor/87-701". aerialvisuals.ca. Retrieved 13 May 2022.
- ^ Baker 1995, pp. 28–29, 32.
- ^ Aronstein 1998, pp. 131, 154.
Bibliography
- "ATF procurement launches new era". ISSN 0015-3710. Archived from the originalon 24 July 2012. Retrieved 24 June 2011.
- "Pentagon relaxes ATF design secrecy". ISSN 0015-3710. Archived from the originalon 5 November 2012. Retrieved 24 June 2011.
- "Lockheed'S ATF Stresses Agility". ISSN 0015-3710. Archived from the originalon 5 November 2012. Retrieved 23 June 2011.
- "YF-22 flies as ATFs head for deadline". ISSN 0015-3710. Archived from the originalon 21 May 2011. Retrieved 23 June 2011.
- Bailey, John (5–11 September 1990). "YF-22 ATF prototype set for maiden flight". ISSN 0015-3710. Archived from the originalon 5 November 2012. Retrieved 23 June 2011.
- Baker, David (January 1995). "From ATF to Lightning II: A Bolt in Anger: Part Two: Lockheed's YF-22A". ISSN 0306-5634.
- Goodall, James C. (1992). "The Lockheed YF-22 and Northrop YF-23 Advanced Tactical Fighters". America's Stealth Fighters and Bombers, B-2, F-117, YF-22, and YF-23. St. Paul, Minnesota: MBI Publishing Company. ISBN 0-87938-609-6.
- Jenkins, Dennis R.; Landis, Tony R. (2008). Experimental & Prototype U.S. Air Force Jet Fighters. Minnesota, US: Specialty Press. ISBN 978-1-58007-111-6.)
{{cite book}}
: CS1 maint: location missing publisher (link - Miller, Jay (2005). Lockheed Martin F/A-22 Raptor, Stealth Fighter. Hinckley, UK: Midland Publishing. ISBN 1-85780-158-X.
- Pace, Steve (1999). F-22 Raptor, America's Next Lethal War Machine. New York: McGraw-Hill. ISBN 0-07-134271-0.
- Warwick, Graham (6–12 May 1992). "Software suspected in YF-22 ATF accident". ISSN 0015-3710. Archived from the originalon 25 September 2011. Retrieved 24 June 2011.
- Williams, Mel, ed. (2002). Superfighters: The Next Generation of Combat Aircraft. London: AIRtime Publishing. ISBN 1-880588-53-6.
Additional sources
- Aronstein, David C.; Hirschberg, Michael J. (1998). Advanced Tactical Fighter to F-22 Raptor: Origins of the 21st Century Air Dominance Fighter. Arlington, Virginia: American Institute of Aeronautics & Astronomy. ISBN 978-1-56347-282-4.
- Crosby, Francis (2002). Fighter Aircraft. London: Lorenz Books. ISBN 0-7548-0990-0.
- Miller, Jay (1995). Lockheed Martin's Skunk Works: The Official History... Leicester, UK: Midland Publishing. ISBN 1-85780-037-0.
- Pace, Steve (1991). X-Fighters: USAF Experimental and Prototype Fighters, XP-59 to YF-23. Osceola, Wisconsin: Motorbooks International. ISBN 0-87938-540-5.
- ISSN 0192-429X.
- ------- (1998). F-22 Raptor. St. Paul, Minnesota, USA: Motorbooks International Publishing. ISBN 0-7603-0484-X.
- Winchester, Jim, ed. (2005). "Northrop/McDonnell Douglas YF-23". Concept Aircraft: Prototypes, X-Planes, And Experimental Aircraft. The Aviation Factfile. Rochester, Kent, UK: Grange Books. ISBN 1-84013-809-2.