Sunday, February 26, 2012

MiG-35

MiG-35
A MiG-35D
Role Multirole fighter
National origin Russia
Manufacturer Mikoyan
First flight 2007
Status In Development
Number built 3 known completed by June 2010
Developed from Mikoyan MiG-29M
The Mikoyan MiG-35 (Russian: Микоян МиГ-35, NATO reporting name: Fulcrum-F) is a further development of the MiG-29M/M2 and MiG-29K/KUB technology. It is classified as a 4++ generation jet fighter by Mikoyan. The first prototype was a modification of the aircraft that previously served as MiG-29M2 model demonstrator. 10 prototypes have been built so far and are currently subject to extensive field trials. The MiG-35 is now classed as a medium-weight aircraft because its maximum take-off weight has increased by 30 percent, exceeding its previous criteria of classification.
MiG Corporation first officially presented the MiG-35 internationally during the Aero India 2007 air show. The MiG-35 was officially unveiled when the Russian Minister of Defense, Sergey Ivanov, visited Lukhovitsky Machine Building Plant "MAPO-MIG". The single seat version is designated MiG-35 and the two-seat version is MiG-35D. The fighter has vastly improved avionics and weapon systems, notably the new AESA radar and the uniquely designed Optical Locator System (OLS), relieves the aircraft from relying on ground-controlled interception (GCI) systems and enables it to conduct independent multi-role missions.

Development

There have been references in the late-1980s to a very different design also identified as "MiG-35". This design was a single engined combat aircraft for air-to-air and secondary air-to-ground roles. According to unidentified Indian sources the aircraft was evaluated by Indian pilots in the Soviet Union and was probably suggested as an alternative for the Indian LCA being developed at that time.
The MiG-35/MiG-35D exhibits the latest advancements on MiG-29K/KUB and MiG-29M/M2 fighters in combat efficiency enhancement, universality and operational characteristics improvement. The main features of the new design are the fifth-generation information-sighting systems, compatibility with Russian and foreign origin weapons application and an integrated variety of defensive systems to increase combat survivability. The new overall design overtakes the design concepts of the baseline model and enables the new aircraft to conduct full-scale multi-role missions as their western counterparts.
New avionics are intended to help the MiG-35 to gain air superiority as well as to perform all-weather precision ground strikes, aerial reconnaissance with opto-electronic and radar equipment and to conduct complex joint missions. The new aircraft has greater weapons load on nine pylons, increased fuel capacity, better anti-corrosion protection, significantly reduced radar signature and a quadruple-redundant fly-by-wire control system.
Responding to earlier customer criticism, the new design is substantially more reliable than the previous variants. The airframe lifetime and its service life have been extended and it is fitted with new engines with longer mean time between overhauls (MTBO), resulting in a decrease in flight-hour cost of almost 2.5 times compared to those of the old variants. The new engines are now smokeless and include a FADEC type electronic control system for better performance. All aspect vector nozzles which had been demonstrated on MiG-29OVT are also optional.
Other technological improvements were also introduced to enhance the aircraft's ability to conduct independent operations. For example, an airborne oxygen generation plant was added. RAC MiG and the Italian company Elettronica signed a Memorandum of Understanding to provide the MIG-35 with a new multifunction self-protection jammer.
The RAC MiG engineers also developed a set of training simulators to help pilots master the sophisticated controls of the new aircraft. The simulators offer interactive computer-based training systems and offer full-mission motion simulation.
MIG-35D at Aero India 2007
The first demonstrator, a dual-seat aircraft, was built on an existing MiG-29M2 airframe, which previously served as a demonstrator for modifications designated MiG-29MRCA and MiG-29M2.

Unveiling at Aero India

Russia unveiled the MiG-35 at the Aero India 2007 airshow in Bangalore, amid Moscow's keenness to sell these planes to India. It was reported that the MiG-35 made its way from Moscow to Bangalore in less than three hours, assisted by in-flight refueling on the way and flying at supersonic speeds.
The MiG-35 was a contender with the Eurofighter Typhoon, F/A-18E/F Super Hornet, Dassault Rafale, JAS 39 Gripen and F-16 Falcon in the Indian MRCA competition for 126 multirole combat aircraft to be procured by the Indian Air Force. The MiG-35 was ousted from the contest in April 2011.
MIG-35 at MAKS 2009
Aero India 2007 was the first time that the final version of the MiG-35 fighter was displayed in an international air show. Until then, only the prototype of the MiG-35 had been shown to the public at air shows in Russia and the UK in 2005.
It was again demonstrated at Aero India 2009 held at Yelahanka Airbase near Bangalore where it was flown by an Indian Air Force pilot.
By April 2010, pictures and additional info surfaced of two new MiG-35 demonstrators, single-seat MiG-35 bort "961", and two-seat MiG-35D "967". According to Russian media, they have first flown at the beginning of Autumn 2009, and subsequently they took part in MMRCA trials in India starting October 2009. Both have a very high commonality with the previous MiG-29K/KUB airframes, with the immediate visible difference being the braking parachute installed in the place of the hook present on the naval aircraft. Subsequently MiG-35D "967" appears to have been equipped with a similar AESA radar as fitted to the older MiG-35 demonstrator bort "154", identifiable by the dark-grey short nose radome.

Design

The most important changes are the Phazotron Zhuk-AE active electronically scanned array (AESA) radar, the RD-33MK engines and the newly designed Optical Locator System (OLS). Other obvious changes in the cockpit are the reduction in analog electronics.

Power plant

The RD-33MK "Morskaya Osa" (Russian: Морская Оса, literally: "Sea Wasp" or Chironex fleckeri) was installed by the new modification. It is the latest version of the RD-33 and was intended to power the MiG-29K and MiG-29KUB. It has 7% more power compared to the baseline model due to the use of modern materials in the cooled blades, providing a higher thrust of 9,000 kgf. In response to earlier criticism, the new engines are smokeless and include systems that reduce infrared and optical visibility. The engines may be fitted with vectored-thrust nozzles, which would result an increase in combat efficiency by 12% to 15%.
With the vectored thrust nozzles, the engines are designated RD-33OVT and will allow the MiG-35 to be the first production twin-engine aircraft with vectoring nozzles that can pivot in two directions or planes. Other current thrust-vectoring aircraft, such as the Su-30MKI and the F-22, have nozzles that each vector in one plane.

Cockpit

Analogue electronics are minimized, being replaced by 3 equal-size colour liquid-crystal (LCD) mulch-function displays (MFDs) and an additional display for the OLS (the MiG-35D rear cockpit has four LCD s).

Sensors

New modifications include the newly rolled-out Phazotron Zhuk-AE active electronically scanned array (AESA) radar and an optronic complex consisting of the newly designed OLS to replace the previous IRST sensor, an additional OLS under the right air intake, and a pair of laser emission detectors on each wing tip.
The Phazotron Zhuk-AE AESA radar offers a wider range of operating frequencies, providing more resistance to electronic countermeasures (ECM), more detection range, more air and ground targets detected, tracked and able to be engaged simultaneously. The radar is thought to have detection range of 160 km (86 nmi) for air targets and 300 km (160 nmi) for ships.
The OLS, a new development from space technologies, incorporates a helmet-mounted target designation system providing targeting solutions for both ground and air targets in the forward and aft hemispheres of the aircraft. The most vital difference from the previous IRST sensor is that the new device provides not only a better operation range but also offers manually switchable display options of IR view, TV mode or a mix of both that significantly improves man-machine coordination. The OLS on the nose serves as the IRST while the OLS under the right air intake serves as the ground strike designator.
In air combat, the optronic suite allows:
  • Detection of non-afterburning targets at 45 km range and more;
  • Identification of those targets at 8 to 10 km range; and
  • Estimates of aerial target range at up to 15 km.
For ground targets, the suite allows:
  • A tank-effective detection range up to 15 km, and aircraft carrier detection at 60 to 80 km;
  • Identification of the tank type on the 8 to 10 km range, and of an aircraft carrier at 40 to 60 km; and
  • Estimates of ground target range of up to 20 km.
The defensive system equipment consists of radar reconnaissance, electronic countermeasures, and optical systems — notably the laser emission detector on each wingtip — which are able to detect and evaluate the approaching danger and operate decoy dispensers to counteract the approaching threat in the radar and infrared ranges.

Open architecture

The final configuration of the MiG-35's onboard equipment has been left open intentionally using the MIL-STD-1553 bus. The main advantage of an open architecture configuration for its avionics is that future customers will have options to choose from components and systems made by Russian, United States, French and Israeli sources. The Ramenskoe Design Company will act as systems integrator.

Specifications

The MiG-35 is currently in development. Information listed below is preliminary and may change.
Data from Mikoyan MiG-29M2 data, Aero India, airforce-technology, deagel.com, and Rian.ru.
General characteristics
  • Crew: one or two
  • Length: 17.3 m (56 ft 9 in)
  • Wingspan: 12 m (39 ft 4 in)
  • Height: 4.7 m (15 ft 5 in)
  • Wing area: 38 m2 (409 ft2)
  • Empty weight: 11,000 kg (24,250 lb)
  • Loaded weight: 17,500 kg (38,600 lb)
  • Max. takeoff weight: 29,700 kg (65,500 lb)
  • Powerplant: 2 × Klimov RD-33MK afterburning turbofans
    • Dry thrust: 5,400 kgf, 53.0 kN (11,900 lbf) each
    • Thrust with afterburner: 9,000 kgf, 88.3 kN (19,800 lbf) each
Performance
  • Maximum speed: Mach 2.25 (2,400 km/h, 1,491 mph) at altitude; 1,450 km/h (901 mph) at low-level
  • Range: 2,000 km (1,240 mi)
  • Combat radius: 1,000 km (620 mi)
  • Ferry range: 3,100 km (1,930 mi) with 3 external fuel tanks
  • Service ceiling: 17,500 m (57,400 ft)
  • Rate of climb: 330 m/s (65,000 ft/min)
  • Thrust/weight: 1.14
  • Max. maneuvering load factor: 10.0 g
Armament
  • Guns: 1× 30 mm GSh-30-1 cannon, 150 rounds
  • Hardpoints: 9 total (8× under-wing, 1× centre-line)
  • Rockets: S-8, S-13, S-24, S-25L, S-250 unguided and laser-guided rockets
  • Missiles:
    • Air-to-air:
      • AA-10 Alamo: 4× R-27R, R-27T, R-27ER, R-27ET
      • AA-8 Aphid: 4× R-60M
      • AA-11 Archer: 8× R-73E, R-73M, R-74M
      • AA-12 Adder: 8× R-77
    • Air-to-surface:
      • AS-17 Krypton: 4× Kh-31A, Kh-31P
      • AS-14 Kedge: 4× Kh-29T, Kh-29L
  • Bombs:
    • Guided:
      • KAB-500L: 500 kg laser-guided bomb
      • KAB-500T: 500 kg TV-guided bomb
    • Unguided:
      • FAB-250: 250 kg bomb
      • FAB-500: 500 kg bomb
      • ZAB-500 fuel-air explosive Bomb
Avionics
  • Phazotron Zhuk AE AESA radar (or other members of the Zhuk radar family)
  • NII PP OLS-UEM Optical Location station

Friday, February 17, 2012

F-117N

F117" redirects here. For the F117-PW-100 turbofan engine, see Pratt & Whitney PW2000.


F-117 Nighthawk
Top view of angular aircraft banking left while flying over mountain ranges
RoleStealth attack aircraft
National originUnited States
ManufacturerLockheed Corporation
Lockheed Martin
First flight18 June 1981
Introduction15 October 1983
Retired22 April 2008
Primary userUnited States Air Force
Number built64 (5 YF-117As, 59 F-117As)
Unit costUS$42.6 million (flyaway cost)
US$111.2 million (total program)
Developed fromLockheed Have Blue


The Lockheed F-117 Nighthawk was a single-seat, twin-engine stealth ground-attack aircraft formerly operated by the United States Air Force (USAF). The F-117A's first flight was in 1981, and it achieved initial operating capability status in October 1983. The F-117A was "acknowledged" and revealed to the world in November 1988.
A product of Lockheed Skunk Works and a development of the Have Blue technology demonstrator, it became the first operational aircraft initially designed around stealth technology. The F-117A was widely publicized during the Persian Gulf War of 1991. It was commonly called the "Stealth Fighter" although it was a ground-attack aircraft, making its F-designation misleading.
The Air Force retired the F-117 on 22 April 2008. primarily because of the fielding of the F-22 Raptor and the impending introduction of the F-35 Lightning II. Sixty-four F-117s were built, 59 of which were production versions with five demonstrators/prototypes.

Development

 Background and Have Blue

In 1964, Pyotr Ya. Ufimtsev, a Soviet mathematician, published a seminal paper titled Method of Edge Waves in the Physical Theory of Diffraction in the journal of the Moscow Institute for Radio Engineering, in which he showed that the strength of a radar return is related to the edge configuration of an object, not its size. Ufimtsev was extending theoretical work published by the German physicist Arnold Sommerfeld. Ufimtsev demonstrated that he could calculate the radar cross-section across a wing's surface and along its edge. The obvious conclusion was that even a large aircraft could be made stealthy by exploiting this principle. However, the airplane's design would make it aerodynamically unstable, and the state of computer technology in the early 1960s could not provide the kinds of flight computers which allow aircraft such as the F-117, and B-2 Spirit to stay airborne. However, by the 1970s, when a Lockheed analyst reviewing foreign literature found Ufimtsev's paper, computers and software had advanced significantly, and the stage was set for the development of a stealthy airplane.
Aircraft parked inside an open hangar
F-117A painted in "Gray Dragon" experimental camouflage scheme.
The F-117 was born after combat experience in the Vietnam War when increasingly sophisticated Soviet surface-to-air missiles (SAMs) downed heavy bombers. It was a black project, an ultra-secret program for much of its life, until the late 1980s. The project began in 1975 with a model called the "Hopeless Diamond" (a wordplay on the Hope Diamond because of its appearance). The following year, the Defense Advanced Research Projects Agency issued Lockheed Skunk Works a contract to build and test two Stealth Strike Fighters, under the code name "Have Blue". These subscale aircraft incorporated jet engines of the Northrop T-38A, fly-by-wire systems of the F-16, landing gear of the A-10, and environmental systems of the C-130. By bringing together existing technology and components, Lockheed built two demonstrators under budget, at $35 million for both aircraft, and in record time.
The maiden flight of the demonstrators occurred on 1 December 1977. Although both aircraft were lost during the demonstration program, test data proved positive. The success of Have Blue led the government to increase funding for stealth technology. Much of that increase was allocated towards the production of an operational stealth aircraft, the Lockheed F-117A, under the program code name "Senior Trend".

 Senior Trend

The decision to produce the F-117A was made on 1 November 1978, and a contract was awarded to Lockheed Advanced Development Projects, popularly known as the Skunk Works, in Burbank, CaliforniaThe program was led by Ben Rich, who called on Bill Schroeder, a Lockheed mathematician, and Denys Overholser, a computer scientist, to exploit Ufimtsev's work. The three designed a computer program called "Echo", which made it possible to design an airplane with flat panels, called facets, which were arranged so as to scatter over 99% of a radar's signal energy "painting" the aircraft.
The first YF-117A, serial number 79-0780, made its maiden flight from Groom Lake, Nevada on 18 June 1981, only 31 months after the full-scale development decision. The first production F-117A was delivered in 1982, and operational capability was achieved in October 1983. The Air Force denied the existence of the aircraft until 1988, when a grainy photograph was released to the public. In April 1990 two were flown into Nellis Air Force Base, Nevada, arriving during daylight and publicly displayed to a crowd of tens of thousands. Five Full Scale Development (FSD) aircraft were built, designated "YF-117A". The last of 59 production F-117s were delivered on 3 July 1990.
Lockheed F-117.ogg
Play video
 F-117 flight demonstration
As the Air Force has stated, "Streamlined management by Aeronautical Systems Center, Wright-Patterson AFB, Ohio, combined breakthrough stealth technology with concurrent development and production to rapidly field the aircraft... The F-117A program demonstrates that a stealth aircraft can be designed for reliability and maintainability." The aircraft maintenance statistics are comparable to other tactical fighters of similar complexity. Logistically supported by Sacramento Air Logistics Center, McClellan AFB, California, the F-117A was kept at the forefront of technology through a planned weapon system improvement program located at USAF Plant 42 at Palmdale, California.

Designation

The operational aircraft had the official designation of "F-117A". Most modern U.S. military aircraft use post-1962 designations in which the designation "F" is usually an air-to-air fighter, "B" is usually a bomber, "A" is usually a ground-attack aircraft, etc. (Examples include the F-15, the B-2, and the A-6.) The F-117 is primarily a ground-attack aircraft so its "F" designation is inconsistent with the DoD system, but it is an inconsistency that has been repeatedly employed by the U.S. Air Force with several of its ground attack aircraft since the late 1950s, e.g., F-105, F-111, etc.
The designation "F-117" seems to indicate that it was given an official designation prior to the 1962 U.S. Tri-Service Aircraft Designation System and could be considered numerically to be a part of the earlier "Century series" of fighters. The assumption prior to the revealing of the aircraft to the public was that it would likely receive the designation F-19 as that number had not been used. However there were no other aircraft to receive a "100" series number following the F-111. Soviet fighters obtained by the United States via various means under the Constant Peg program were given F-series numbers for their evaluation by U.S. pilots, and with the advent of the Teen Series fighters, most often Century Series designations.
As with other exotic military aircraft types flying in the southern Nevada area, such as captured fighters, an arbitrary radio call of "117" was assigned. This same radio call had been used by the enigmatic 4477th Test and Evaluation Squadron, also known as the "Red Hats" or "Red Eagles", that often had flown expatriated MiGs in the area, but there was no relationship to the call and the formal F-19 designation then being considered by the Air Force. Apparently, use of the "117" radio call became commonplace and when Lockheed released its first flight manual (i.e., the Air Force "dash one" manual for the aircraft), F-117A was the designation printed on the cover.
A televised documentary quoted a senior member of the F-117A development team as saying that the top-notch USAF fighter pilots required to fly the new aircraft were more easily attracted to an aircraft with an "F" designation for fighter, as opposed to a bomber ("B") or attack ("A") designation.

Design

Closeup view of the nose of a black jet, emphasising the many angled-surfaces   Front view of an F-117
The F-117 is shaped to deflect radar signals and is about the size of an F-15 Eagle. The single-seat Nighthawk is powered by two non-afterburning General Electric F404 turbofan engines, and has quadruple-redundant fly-by-wire flight controls. It is air refuelable. To lower development costs, the avionics, fly-by-wire systems, and other parts are derived from the General Dynamics F-16 Fighting Falcon, McDonnell Douglas F/A-18 Hornet and McDonnell Douglas F-15E Strike Eagle. The parts were originally described as spares on budgets for these aircraft, to keep the F-117 project secret.
The F-117 Nighthawk has a radar signature of about 0.025 m2 (0.269 sq ft). Among the penalties for stealth are lower engine power thrust, due to losses in the inlet and outlet, a very low wing aspect ratio, and a high sweep angle (50°) needed to deflect incoming radar waves to the sides. With these design considerations and no afterburner, the F-117 is limited to subsonic speeds. It also has serrated edges in places to scatter as much radar signals.
The F-117A is equipped with sophisticated navigation and attack systems integrated into a digital avionics suite. It carries no radar, which lowers emissions and cross-section. It navigates primarily by GPS and high-accuracy inertial navigation. Missions are coordinated by an automated planning system that can automatically perform all aspects of an attack mission, including weapons release. Targets are acquired by a thermal imaging infrared system, slaved to a laser that finds the range and designates targets for laser-guided bombs. The F-117A's split internal bay can carry 5,000 lb (2,300 kg) of ordnance. Typical weapons are a pair of GBU-10, GBU-12, or GBU-27 laser-guided bombs, two BLU-109 penetration bombs, or two Joint Direct Attack Munitions (JDAMs), a GPS/INS guided stand-off bomb.

Operational history

Look-down view of four black aircraft flying in formation, three of which fly behind and underneath the lead aircraft.
F-117s in formation
During the program's early years, from 1984 to mid-1992, the F-117A fleet was based at Tonopah Test Range Airport, Nevada where it served under the 4450th Tactical Group. Because the F-117 was classified during this time, the 4450th Tactical Group was "officially" located at Nellis Air Force Base, Nevada and equipped with A-7 Corsair II aircraft. The 4450th was absorbed by the 37th Tactical Fighter Wing in 1989. In 1992, the entire fleet was transferred to Holloman Air Force Base, New Mexico, where it was placed under the command of the 49th Fighter Wing. This move also eliminated the Key Air and American Trans Air contract flights to Tonopah, which flew 22,000 passenger trips on 300 flights from Nellis to Tonopah per month.
F-117 pilots called themselves "Bandits". Each of the 558 Air Force pilots who have flown the F-117 have a Bandit number, such as "Bandit 52", that indicates the sequential order of their first flight in the F-117.
The F-117 has been used several times in war. Its first mission was during the United States invasion of Panama in 1989. During that invasion two F-117A Nighthawks dropped two bombs on Rio Hato airfield.
During the Persian Gulf War in 1991, the F-117A flew approximately 1,300 sorties and scored direct hits on 1,600 high-value targets in Iraq over 6,905 flight hours. Only 2.5% of the American aircraft in Iraq were F-117s, yet they struck more than 40% of the strategic targets. F-117As dropped over 2,000 tons of precision-guided munitions and struck their targets with over an 80% success rate. "Although the 37th Tactical Fighter Wing Provisional and its 42 stealth fighters represented just 2.5 percent of all allied fighter and attack aircraft in the Persian Gulf, the F-117As were assigned against more than 31 percent of the strategic Iraqi military targets attacked during the first 24 hours of the air campaign."
Lockheed F-117 Nighthawk.ogv
Play video
F-117 Nighthawk USAF video
It was one of very few U.S. or Coalition aircraft types to strike targets in downtown Baghdad. Its stealth characteristics protected it from the SAM and AAA-saturated environment of the city, and due both to its precision-guided weaponry and its avoidance of having to jettison ordnance in defensive maneuvers F-117 missions proved less likely to cause civilian casualties and collateral damage.
Following its move to Holloman AFB in 1992, the F-117A and the men and women of the 49th Fighter Wing were deployed to Southwest Asia on multiple occasions. On their first deployment, crews flew non-stop from Holloman to Kuwait, a flight of approximately 18.5 hours – a record for single-seat fighters that stands today.
The F-117 was subsequently used in Operation Allied Force in 1999, Operation Enduring Freedom in 2001, and Operation Iraqi Freedom in 2003.

Combat loss

Only one F-117 (AF ser. no. 82-0806) was lost to enemy action. It was shot down during a mission against the Army of Yugoslavia on 27 March 1999, during Operation Allied Force. About 8:15 pm local time, SA-3s were fired from about 8 miles (13 km) away, launched by a Yugoslav version of the Soviet Isayev S-125 "Neva" (NATO name SA-3 "Goa") anti-aircraft missile system. The launcher was run by elements of the 3rd Battalion of the 250th Air Defence Missile Brigade under the command of Colonel Zoltán Dani.According to NATO Commander Wesley Clark and other NATO generals, Dani detected F-117s by operating his radars on unusually long wavelengths, making the aircraft visible for brief periods. According to Dani in a 2007 interview, his troops spotted the aircraft on radar when its bomb-bay doors opened, raising its radar signature. One of the missiles detonated near the F-117 by its proximity fuze. Dani said he kept most of his missile sites intact by frequently moving them, and had spotters looking for F-117s and other NATO aircraft. He oversaw the modification of his targeting radar to improve its detection. He later recanted this claim, saying that it was meant as a tongue-in-cheek jab to his former American adversaries and their customary boastfulness.

Canopy of F-117 shot down in Serbia in March 1999 at the Museum of Aviation in Belgrade
After the explosion, the aircraft became uncontrollable, forcing the pilot to eject. The pilot was recovered a short time later by a U.S. Marine Corps combat search and rescue team. Photos show that the aircraft struck the ground at low speed in an inverted position, and that the airframe remained relatively intact. U.S. forces decided not to bomb the wreckage because civilians were near. The Serbs are believed to have invited Russian personnel to inspect the aircraft's remains, compromising the then 25-year-old U.S. stealth technology.
The F-117's pilot was initially misidentified. While the name "Capt Ken 'Wiz' Dwelle" was painted on the canopy, it was revealed in 2007 that the pilot was actually Lt Col Dale Zelko, USAF.

Retirement

Though advanced for its time, the F-117's stealthy faceted airframe required a large amount of maintenance and was eventually superseded by streamlined shapes produced with computer-aided design. The Air Force had once planned to retire the F-117 in 2011, but Program Budget Decision 720 (PBD 720), dated 28 December 2005, proposed retiring it by October 2008 to free up an estimated $1.07 billion to buy more F-22 Raptors. PBD 720 called for 10 F-117s to be retired in FY 2007 and the remaining 42 in FY 2008, stating that other Air Force planes and missiles could stealthily deliver precision payloads, including the B-2 Spirit, F-22 and JASSM.
In late 2006, the Air Force closed the F-117 formal training unit (FTU), and announced the retirement of the F-117. The first six aircraft to be retired made their last flight on 12 March 2007 after a ceremony at Holloman AFB to commemorate the aircraft's career. Brigadier General David Goldfein, commander of the 49th Fighter Wing, said at the ceremony, "With the launch of these great aircraft today, the circle comes to a close – their service to our nation's defense fulfilled, their mission accomplished and a job well done. We send them today to their final resting place – a home they are intimately familiar with – their first, and only, home outside of Holloman."

A pair of specially painted F-117 Nighthawks fly off from their last refueling by the Ohio Air National Guard's 121st Air Refueling Wing.
Unlike most other Air Force aircraft which are retired to Davis-Monthan AFB for scrapping, or dispersal to museums, most of the F-117s were retired to their original hangars at the Tonopah Test Range Airport. At Tonopah, their wings were removed and the aircraft are stored in their original climate-controlled hangars. The decommissioning occurred in eight phases, with the operational aircraft retired to Tonapah in seven waves beginning on 13 March 2007, and ending with the last wave's arrival on 22 April 2008.Four aircraft were kept flying beyond April by the 410th Flight Test Squadron at Palmdale for flight test. By the beginning of August, two were remaining. The last F-117 (AF ser. no. 86-0831) left Palmdale to fly to Tonopah on 11 August 2008. This was the last flight of an F-117.With the last aircraft retired, the 410th was deactivated in a ceremony on 1 August 2008.
Through 2009, one F-117 had been scrapped. AF ser. no. 79-0784 was scrapped at the Palmdale test facility on 26 April 2008. The aircraft was the last F-117 at Palmdale and was scrapped to test an effective method for destroying F-117 airframes.
Although officially retired, the F-117 fleet remains intact, and photos show the aircraft carefully mothballed. No further aircraft have been scrapped, or transferred to museums.

Variants

 F-117N “Seahawk”

In the early 1990s, Lockheed proposed an upgraded, carrier capable variant of the F-117 dubbed the “Seahawk” to the U.S. Navy as an alternative to the canceled A/F-X program. The unsolicited proposal was received poorly by the Department of Defense, which had little interest in the single mission capabilities of such an aircraft, particularly as it would take money away from the Joint Advanced Strike Technology program, which evolved into the Joint Strike Fighter. The new aircraft would have differed from the land-based F-117 in several ways, including the addition “of elevators, a bubble canopy, a less sharply swept wing and reconfigured tail".The “N” variant would also be re-engined to use General Electric F414 turbofans instead of the older General Electric F404s. Furthermore the aircraft would be optionally fitted with hardpoints, allowing for an additional 8,000 lb (3,600 kg) of payload, and a new ground attack radar with air-to-air capability. In that role the F-117N could carry AIM-120 AMRAAM air-to-air missiles.
After being rebuffed by the Navy, Lockheed submitted an updated proposal that included afterburning capability and a larger emphasis on the F-117N as a multi-mission aircraft, rather than just an attack aircraft. In efforts to boost interest, Lockheed also proposed an F-117B land-based variant that shared most of the F-117N capabilities. This variant was proposed to both the US Air Force and the Royal Air Force.This renewed F-117N proposal was also known as the A/F-117X. Neither the F-117N or the F-117B were purchased by any party.                                                                                                                               From Wikipedia, the free encyclopedia

World's Most Dangerous Air Port

Tenzing-Hillary Airport (IATA: LUA, ICAO: VNLK), also known as Lukla Airport, is a small airport in the town of Lukla, in Khumbu, Solukhumbu district, Sagarmatha zone, eastern Nepal. A program entitled Most Extreme Airports broadcast on The History Channel in 2010, rated the airport as the most dangerous airport in the World. In January 2008, the airport was renamed in honor of Sir Edmund Hillary and Sherpa Tenzing Norgay, the first persons to reach the summit of
Mount Everest and also to mark their efforts in the construction of this airport.
The airport is popular because Lukla is the place where most people start the climb to Mount Everest Base Camp. There are daily flights between Lukla and Kathmandu during daylight hours, in good weather. Although the flying distance is short, rain commonly occurs in Lukla while the sun is shining brightly in Kathmandu. High winds, cloud cover and changing visibility often mean flights can be delayed or the airport closed completely. The airport is contained within a chain link fence and patrolled by the Nepal armed police or civil police around the clock. The airport finished eighth in a poll by PrivateFly.com, in 2010, to find the world's best airport approaches.
Facilities
The airport's paved asphalt runway is only accessible to helicopters and small, fixed-wing, short-takeoff-and-landing aircraft, such as the De Havilland Canada DHC-6 Twin Otter or Dornier Do 228. Tara Air also operates two Pilatus PC-6 Turbo Porter aircraft, that visit Lukla on a charter basis. The single runway is 1,500 feet (460 m) long, 65 feet (20 m) wide and has a 12% gradient. The elevation of the airport is 9,100 feet (2,800 m).
Aircraft can only use runway 06 for landings and runway 24 for takeoffs. Due to the terrain, there is no prospect of a successful go-around on short final. There is high terrain immediately after the northern end of the runway and a steeply angled drop, of about 2,000 feet (610 m) at the southern end of the runway, into the valley below.
The apron has four stands and there is one helipad located 450 feet (140 m) from the control tower. No landing aids are available and the only air traffic service is an Aerodrome Flight Information Service.

Airlines and destinations



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AirlinesDestinations
Agni AirKathmandu
Gorkha AirlinesKathmandu
Nepal AirlinesKathmandu, Kangel Danda, Lamidanda, Phaplu, Rumjatar
Sita AirKathmandu
Tara AirKathmandu

Incidents and accidents

  • On 15 October 1973, on landing at the airport, a Royal Nepal Airlines DHC-6 Twin Otter 300, registration 9N-ABG, was damaged beyond repair. The three crew and three passengers were unhurt.
  • On 9 June 1991, flying from Kathmandu, a Royal Nepal Airlines DHC-6 Twin Otter 300, registration 9N-ABA, crashed at the airport while attempting to land following an unstabilized approach in bad weather. All three crew and fourteen passengers were unhurt.
  • On 26 September 1992, a Royal Air Nepal Harbin Yunshuji Y-12-11 registered 9N-ACI faltered during take-off and was damaged beyond repair. All on board (twelve passengers and two crew) survived.
  • On 25 May 2004, while on approach to the airport, a Yeti Airlines DHC-6 Twin Otter Series 300 (registration 9N-AFD) flying from Kathmandu crashed into Lamjura Hill in heavy cloud. No passengers were on board, but all three crew members were killed. The Nepalese accident investigation committee concluded that the captain provided inaccurate information as regards his position to the Area Control Centre.
  • On 1 October 2004, on landing at the airport, a Sita Air Dornier Do 228 suffered a collapse of its nose gear and slid along the runway, blocking it once it had come to rest. The airport was closed for two days.
  • On 30 June 2005, a Gorkha Airlines Dornier Do 228 skidded off the runway while attempting to land. The nine passengers and three crew suffered minor injuries. The aircraft was reportedly withdrawn from use and written off after the accident.
  • On 8 October 2008, Yeti Airlines Flight 103, a DHC-6 Twin Otter, crashed on final approach and caught fire, killing eighteen passengers and crew. The aircraft's captain was the only survivor.
  • On 25 August 2010, Agni Air Flight 101 crashed at Shikharpur while returning to Kathmandu after bad weather had prevented it from reaching Lukla. All eleven passengers and three crew perished.
  • On 12 October 2010, a Sita Air Dornier Do 228 (registration 9N-AHB) lost braking control and impacted the wall-end of the runway during landing. All passengers and crew on board survived without injuries and the aircraft received damage to its nose.

     

Thursday, February 9, 2012

Tuesday, February 7, 2012

Red Arrows

The Red Arrows, officially known as the Royal Air Force Aerobatic Team, is the aerobatics display team of the Royal Air Force based at RAF Scampton, but due to move to RAF Waddington in 2011. The team was formed in late 1964 as an all-RAF team, replacing a number of unofficial teams that had been sponsored by RAF commands.
The Red Arrows badge shows the aircraft in their trademark diamond nine formation, with the motto Éclat, a French word meaning "brilliance" or "excellence".
Initially, they were equipped with seven Folland Gnat trainers inherited from the RAF Yellowjacks display team. This aircraft was chosen because it was less expensive to operate than front-line fighters. In their first season, they flew at 65 shows across Europe. In 1966, the team was increased to nine members, enabling them to develop their Diamond Nine formation. In late 1979, they switched to the BAE Hawk trainer. The Red Arrows have performed over 4,000 displays worldwide in 53 countries.
Team history

Predecessors


Red Arrow at speed with red smoke on, 2010
The Red Arrows were not the first RAF aerobatics team. An RAF biplane pageant was held at Hendon in 1920 with biplane teams from front-line squadrons. In 1938, three Gloster Gladiators flew with their wing-tips tied together. The Second World War largely stopped formation aerobatics, as planes were needed elsewhere.
In 1947, the first jet team of three de Havilland Vampires came from Odiham Fighter Wing. Various teams flew the Vampire, and in 1950, No. 72 Squadron was flying a team of seven. No. 54 Squadron RAF became the first RAF jet formation team to use smoke trails. Vampires were replaced by Meteors, No 66 Squadron developing a formation team of six aircraft.
Hunter aircraft were first used for aerobatics teams in 1955, when No 54 Squadron flew a formation of four.
The official RAF team was provided by No. 111 Squadron RAF ('Treblers' or 'Treble-One') in 1956, and for the first time the aircraft had a special colour scheme, which was an all-black finish. After a demonstration in France, they were hailed as "Les Fleches Noires" and from then on known as the Black Arrows. This team became the first team to fly a five-Hunter formation. The Black Arrows' greatest moment was the loop and barrel roll of 22 Hunters during the 1958 Farnborough Airshow. This was a world record for the greatest number of aircraft looped in formation, and remains unbroken to this day. The Black Arrows were the premier team until 1961, when the Blue Diamonds (No. 92 Squadron RAF) continued their role, flying sixteen blue Hunters.
In 1960, the Tigers (No. 74 Squadron RAF) were re-equipped with the supersonic English Electric Lightning and performed wing-overs and rolls with nine aircraft in tight formation. They sometimes gave co-ordinated displays with the Blue Diamonds.
Yet another aerobatics team was formed by No. 56 Squadron RAF, the Firebirds, with nine red and silver Lightnings. In 1964, the Red Pelicans, flying six BAC Jet Provost T Mk 4s, assumed the role of the RAF's leading display team. In that same year, a team of five yellow Gnat trainers from No 4 Flying Training School displayed at the Farnborough Airshow. This team became known as the Yellowjacks after Flight Lieutenant Lee Jones's call sign, "Yellowjack"; the name was briefly 'Daffodil Patrol', but was quickly changed back.
In 1964, all the RAF display teams were amalgamated, as it was feared pilots were spending too much time practising formation aerobatics rather than operational training. The new team name took the word red from the fact that the Yellowjacks' planes had been painted red (for safety reasons, as it was a far clearer and more visible colour in the sky) and arrows after the Black Arrows; the official version, however, is that the red was a tribute to the Red Pelicans.Another reason for the change to red was that responsibility for the team moved from Fighter Command to the Central Flying School, whose main colour was red.

Establishment


A Red Arrows pilot exits his Hawk aircraft at the end of the display
The Royal Air Force Aerobatic Team, the Red Arrows, was based at RAF Kemble, then a satellite unit of the Central Flying School, itself based at RAF Little Rissington, which was considered the "official" home base of the Arrows. Arrows' aircraft would frequently fly into Rissington for maintenance. When RAF Scampton became the CFS Headquarters in 1983, the Red Arrows moved there. As an economy measure, Scampton closed in 1995, so the Red Arrows moved just twenty miles to RAF Cranwell; however, as they still used the air space above Scampton, the emergency facilities and runways had to be maintained. Since 21 December 2000, the Red Arrows have been based again at RAF Scampton, near Lincoln.

The Red Arrows escort Concorde at the Queen's Golden Jubilee flyover of London
The first team, led by Squadron Leader Lee Jones, had seven display pilots and flew the Folland Gnat T1 jet trainer. The first display in the UK was on 6 May 1965 at Little Rissington for a press day. At the subsequent National Air Day display, three days later, at Clermont Ferrand in France, one French journalist described the team as "Les Fleches Rouges", confirming the name "The Red Arrows". By the end of their first season, the Red Arrows had displayed 65 times in Britain, France, Italy, Holland, Germany and Belgium and were awarded the Britannia Trophy by the Royal Aero Club for their contribution to aviation.
In 1968, the then Team Leader (Sqn Ldr Ray Hanna) expanded the team from seven to nine jets, as he wanted to expand the team's capabilities and the permutations of formation patterns. It was during this season that the 'Diamond Nine' pattern was formed and it has remained the team's trademark pattern ever since. Ray Hanna served as Red Leader for three consecutive years until 1968 and was recalled to supersede Squadron Leader Timothy Nelson for the 1969 display season, a record four seasons as Leader which still stands to this day. For his considerable achievements of airmanship with the team, Ray Hanna was awarded a bar to his existing Air Force Cross (AFC).
After displaying 1,292 times in the Folland Gnat, the Red Arrows took delivery of the BAe Hawk in the winter of 1979. Since being introduced into service with the Red Arrows, the Hawk has performed with the Red Arrows in fifty countries.

Folland Gnat T1 on display in 2009 in Red Arrows markings at the former team base Kemble.
In July 2004 there was speculation in the British media that the Red Arrows would be disbanded, after a defence spending review, due to running costs of between £5 million and £6 million. The Arrows were not disbanded and their expense has been justified through their public relations benefit of helping to develop business in the defence industry and promoting recruitment for the RAF. According to the BBC, it is highly unlikely that the Red Arrows will be disbanded, as they are a considerable attraction throughout the world. This was reiterated by then Prime Minister, Tony Blair, in 2007.
With the planned closure of RAF Scampton, the future home of the Red Arrows became uncertain. On 20 May 2008 months of speculation was ended when it was revealed that the Ministry of Defence were moving the Red Arrows to nearby RAF Waddington.

Pilots


The pilots line up for an official photo after their display in 2004
Since 1966, there have been nine display pilots each year, all volunteers. Pilots must have completed one or more operational tours on a fast jet such as the Tornado, Harrier or Jaguar, have accumulated at least 1,500 flying hours and have been assessed as above average in their operational role to be eligible. Even then, there are more than ten applicants for each place on the team.Pilots stay with the Red Arrows for a three-year tour of duty. Three pilots are changed every year, such that there are always three first year pilots, three second year pilots, and three in their final year.
The Reds have no reserve pilots, as a spare pilot would not perform often enough to fly to the standard required. If one of the pilots is not able to fly, the team flies an eight-plane formation. However, if the Team Leader, 'Red 1', is unable to fly then the team does not display at all. Each pilot always flies the same position in a formation. The pilots spend six months from October to April practising for the display season. Pilots wear green flying suits during training, and are only allowed to wear their red flying suits when fully qualified.
During an aerobatics display, Red Arrows pilots experience forces up to five times that of gravity (1g), and when performing the aerobatic manoeuvre 'Vixen Break', forces up to 7g can be reached, close to the 8g structural limit of the aircraft.
As well as the nine pilots, 'Red 10', also known as the Road Manager, is a fully qualified Hawk pilot who flies the tenth aircraft when the Red Arrows are away from base. This means the team have a reserve aircraft at the display site. Red 10's duties include co-ordination of the display and acting as the team's Ground Safety Officer. Red 10 also flies TV cameramen and photographers for air-to-air pictures of the Red Arrows. The engineering team that supports the Red Arrows is known as "The Blues" and consists of 85 members.

Red Arrows at Southport Airshow in 2009
On 13 May 2009, it was announced that the Red Arrows would include their first female display pilot. Flt Lt Kirsty Moore joined for the 2010 season alongside fellow newcomer Flt Lt Ben Plank. Wing Commander Jas Hawker concluded his three year tour of duty as 'The Boss' and was replaced by 2009 Red Six, Squadron Leader Ben Murphy.Flt Lt Moore is not the first female to apply to become a Red Arrow, but is the first to be taken forward to the intense selection. She joined the RAF in 1998 and has been an instructor on the Hawk aircraft at RAF Valley. She flies the Tornado aircraft at RAF Marham.Flt Lt Plank is based at RAF Cottesmore.
The team for the 2011 season was announced on 13 September 2010 and subsequently undertook winter training in preparation for the 2011 display season. The team departed the UK on Friday 18 March 2011 and travelled to Cyprus to undertake Exercise SPRINGHAWK at RAF Akrotiri. The first 9-ship practice was flown on the first day of training in Cyprus on Monday 21 March 2011. The team remained in Cyprus until the end of May whilst they took advantage of the good weather on offer to work up to display standard. The team gained their PDA (Public Display Authority) on Thursday 20 May 2011 just two days before their first planned public display in Crete.

Aircraft


BAE Hawk T1A of the Red Arrows taxis after landing
The Red Arrows do not use front-line aircraft because of operating costs. The team uses the RAF's advanced jet trainer, the BAE Hawk T1A, built at Brough in the East Riding of Yorkshire. While the Hawk is very basic compared to the much more modern Eurofighter Typhoon, it is still fast enough and very manoeuvrable, ideal for low-altitude aerobatics. The plane does not have a sat nav, radar or onboard computer. The Red Arrows normally cruise at 360 knots (one nautical mile every 10 seconds).

Displays


The Red Arrows in formation with two Supermarine Spitfires at RIAT 2005
The first display by the Red Arrows was at RAF Little Rissington on 6 May 1965. The display was to introduce the Royal Air Force Aerobatic Team to the media. However, the first public display was on 9 May 1965 in France, at the French National Air Day in Clermont-Ferrand. The first public display in the UK was on 15 May 1965 at the Biggin Hill International Air Fair. The first display with nine aircraft was on 8 July 1966 at RAF Little Rissington.
The first display in Germany was at RAF Laarbruch on 6 August 1965. The Red Arrows performed in Germany a further 170 times before formation aerobatics were banned in Germany following the Ramstein airshow disaster in 1988.

Part of the "Big Vixen" formation
During displays, the aircraft do not fly directly over the crowd apart from entering the display area by flying over the crowd from behind; any manoeuvres in front of and parallel to the audience can be as low as 300 feet, the 'synchro pair' can go as low as 100 feet straight and level, or 150 feet when in inverted flight. To carry out a full looping display the cloud base must be above 4,500 feet to avoid the team entering the cloud while looping If the cloud base is less than 4,500 ft but more than 2,500 ft the Team will perform the Rolling Display, substituting wing-overs and rolls for the loops. If the cloud base is less than 2,500 ft the Team will fly the Flat Display, which consists of a series of fly-pasts and steep turns.
One of the biggest crowds to see the Red Arrows was in Lisbon on 13 June 1973, when there was a crowd of 650,000 people, a statistic exceeded in 1996 in Sydney.
The greatest number of displays flown in any year was in 1995, when the Red Arrows performed 136 times. The smallest number of displays in one year was in 1975, after the 1973 oil crisis limited their appearances.
At a charity auction, a British woman paid £1.5 million to fly with them.
By the end of the 2009 season, the Red Arrows had performed a total of 4,269 displays in 53 countries. The 4,000th display was at RAF Leuchars during the Battle of Britain Airshow in September 2006.

Display charges

In 1977, a charge of £200 was introduced by the MOD for a Red Arrows display. By 2000, the charge had risen to £2,000 (including VAT and insurance). In 2011 the team manager quoted the charge as £9,000.

Transits

On a transit flight (getting to or from a display location) the team may fly at the relatively low altitude of 1,000 feet (300 m). This avoids the complication of moving though the cloud base in formation, and also avoids much controlled air space. Jets are more efficient at higher altitude, so longer flights are made at 35,000 to 42,000 feet (11,000 to 13,000 m). On transit flights, the formation can include spare planes. Sometimes a C-130 Hercules accompanies them, carrying spare parts.
As the fuel tank capacity of the Hawk sets a limit to flight distance, very long transits between display sites may need landings on the way to refuel. For example, travel to Canada has required refuelling stops in Iceland and Greenland.

Smoke


The Red Arrows in Apollo formation, 2010
The smoke trails left by the team are made by releasing diesel into the exhaust; this oxidises straight away, leaving a white smoke trail. Dyes can be added to produce the red and blue colour. The diesel is stored in the pod on the underside of the plane; it houses three tanks: one 50-imperial-gallon (230 L) tank of pure diesel and two 10-imperial-gallon (45 L) tanks of blue- and red-dyed diesel. The smoke system uses 10-imperial-gallon (45 L) per minute; therefore each plane can trail smoke for a total of seven minutes – 5 minutes of white smoke, 1 minute of blue and 1 minute of red.

From Wikipedia, the free encyclopedia

Monday, February 6, 2012

F-22 Raptor


F-22 Raptor
F-22 Raptor banking left in-flight, showing the top view of the aircraft. The engines with afterburners emit a pinkish glow. Aircraft mostly gray, apart from the gold cockpit window, with hints of bluish condensation on the wings.
The F-22 Raptor
RoleStealth air superiority fighter
National originUnited States
ManufacturerLockheed Martin Aeronautics
Boeing Defense, Space & Security
First flight7 September 1997
Introduction15 December 2005
StatusIn service, out of production
Primary userUnited States Air Force
Produced1997-2011
Number built195 (8 test and 187 operational) aircraft
Program costUS$66.7 billion
Unit costUS$150 million (flyaway cost for FY2009)
Developed fromLockheed YF-22
Developed intoLockheed Martin X-44 MANTA
Lockheed Martin FB-22


The Lockheed Martin/Boeing F-22 Raptor is a single-seat, twin-engine fifth-generation supermaneuverable fighter aircraft that uses stealth technology. It was designed primarily as an air superiority fighter, but has additional capabilities that include ground attack, electronic warfare, and signals intelligence roles. Lockheed Martin Aeronautics is the prime contractor and is responsible for the majority of the airframe, weapon systems and final assembly of the F-22. Program partner Boeing Defense, Space & Security provides the wings, aft fuselage, avionics integration, and training systems.
The aircraft was variously designated F-22 and F/A-22 during the years prior to formally entering USAF service in December 2005 as the F-22A. Despite a protracted and costly development period, the United States Air Force considers the F-22 a critical component of US tactical air power, and claims that the aircraft is unmatched by any known or projected fighter, while Lockheed Martin claims that the Raptor's combination of stealth, speed, agility, precision and situational awareness, combined with air-to-air and air-to-ground combat capabilities, makes it the best overall fighter in the world today. Air Chief Marshal Angus Houston, former Chief of the Australian Defence Force, said in 2004 that the "F-22 will be the most outstanding fighter plane ever built."
The high cost of the aircraft, a lack of clear air-to-air combat missions because of delays in the Russian and Chinese fifth-generation fighter programs, a US ban on Raptor exports, and the ongoing development of the planned cheaper and more versatile F-35 resulted in calls to end F-22 production. In April 2009 the US Department of Defense proposed to cease placing new orders, subject to Congressional approval, for a final procurement tally of 187 operational aircraft. The National Defense Authorization Act for Fiscal Year 2010 lacked funding for further F-22 production. The final F-22 rolled off the assembly line on 13 December 2011 during a ceremony at Dobbins Air Reserve Base

 


Development

Origins

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 influenced by the emerging worldwide threats, including development and proliferation of Soviet Su-27 "Flanker"- and MiG-29 "Fulcrum-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. A request for proposals (RFP) was issued in July 1986, and two contractor teams, Lockheed/Boeing/General Dynamics and Northrop/McDonnell Douglas were selected on 31 October 1986 to undertake a 50-month demonstration phase, culminating in the flight test of two prototypes, the YF-22 and the YF-23.
Each design team produced two prototypes featuring one of two engine options, one featuring thrust vectoring. The Pratt & Whitney F119 turbofan with vectored thrust permits a tighter turning radius, a valuable capability in dogfights. During the development process, the ATF's increasing weight and cost drove out some features. A dedicated infra-red search and track (IRST) system was downgraded from multi-color to single color then deleted, the side-looking radars were deleted and the ejection seat requirement was downgraded from a fresh design to the existing McDonnell Douglas ACES II.
On 23 April 1991, the YF-22 was announced by Secretary of the Air Force Donald Rice as the winner of the ATF competition.The YF-23 design was more stealthy and faster, but the YF-22 was more agile.The aviation press speculated that the YF-22 was also more adaptable to the Navy's Navalized Advanced Tactical Fighter (NATF), but the US Navy abandoned NATF by 1992.In 1991, the Air Force planned to buy 650 aircraft.

Production and procurement


The first operational F-22 Raptor is painted at the Lockheed Martin assembly plant at Marietta, Georgia
The production F-22 model was unveiled on 9 April 1997 at Lockheed Georgia Co., Marietta, Georgia. It first flew on 7 September 1997. The first production F-22 was delivered to Nellis Air Force Base, Nevada, on 7 January 2003. In 2006, the Raptor's development team, composed of Lockheed Martin and over 1,000 other companies, plus the United States Air Force, won the Collier Trophy, American aviation's most prestigious award.In 2006, the USAF sought to acquire 381 F-22s, to be divided among seven active duty combat squadrons and three integrated Air Force Reserve Command and Air National Guard squadrons.
Several design changes were made from the YF-22 for production. The swept-back angle on the wing's leading edge was decreased from 48° to 42°, while the vertical stabilizer area was decreased by 20%. To improve pilot visibility, the canopy was moved forward 7 inches (178 mm), and the engine intakes were moved rearward 14 inches (356 mm). The shape of the wing and stabilator trailing edges was refined to improve aerodynamics, strength, and stealth characteristics.Also, the vertical stabilizer was shifted rearward.
F-22 production was split up over many subcontractors across 46 states, in a strategy to increase Congressional support for the program.However the production split, along with the use of several new technologies were likely responsible for increased costs and delays.[ Many capabilities were deferred to post-service upgrades, reducing the initial cost but increasing total project cost.Each aircraft required "1,000 subcontractors and suppliers and 95,000 workers" to build.The F-22 was in production for 15 years, at a rate of roughly two per month.
Two F-22s overflying snow-capped mountains.
Two F-22s during flight testing, the upper one being the first EMD F-22, "Raptor 01"
The United States Air Force originally planned to order 750 ATFs at a cost of $26.2 billion, with production beginning in 1994; however, the 1990 Major Aircraft Review led by Defense Secretary Dick Cheney altered the plan to 648 aircraft beginning in 1996. The goal changed again in 1994, when it became 438 aircraft entering service in 2003 or 2004, but a 1997 Department of Defense report put the purchase at 339. In 2003, the Air Force said that the existing congressional cost cap limited the purchase to 277. By 2006, the Pentagon said it will buy 183 aircraft, which would save $15 billion but raise the cost of each aircraft, this was implemented in the form of a multi-year procurement plan, which allowed for further orders later. The total cost of the program by 2006 was $62 billion.
In April 2006, the cost of the F-22 was assessed by the Government Accountability Office to be $361 million per aircraft. By April 2006, $28 billion had been invested in F-22 development and testing; while the Unit Procurement Cost was estimated at $177.6 million in 2006, based on a production run of 181 airframes. It was estimated by the end of production, $34 billion will have been spent on procurement, resulting in a total program cost of $62 billion, around $339 million per aircraft. The incremental cost for an additional F-22 was estimated at about $138 million.

Two F-22 Raptors line up for refueling during their first official deployment, October 2005
On 31 July 2007, Lockheed Martin received a multi-year contract for 60 F-22s worth a total of $7.3 billion. The contract brought the number of F-22s on order to 183 and extended production through 2011. If production were restarted the cost for another 75 aircraft was estimated in 2009 to be an extra $70 million per unit.

Ban on exports

No opportunity for export currently exists because the export sale of the F-22 is barred by American federal law. Current customers for U.S. fighters are either acquiring earlier designs such as the F-15, F-16 Fighting Falcon, and Boeing F/A-18E/F Super Hornet, or are waiting to acquire the Lockheed Martin F-35 Lightning II (Joint Strike Fighter), which contains technology from the F-22 but is designed to be cheaper, more flexible, and available for export. The F-35 will not be as agile as the F-22 or fly as high or as fast, but its radar and avionics will be more advanced.On 27 September 2006, Congress upheld the ban on foreign sales of the F-22; and confirmed this in December 2006.
The Japanese government showed interest in the F-22 for its Replacement-Fighter program. However, a sale would need approval from the Pentagon, State Department and Congress. It was stated that the F-22 would decrease the number of fighters needed by the Japan Air Self-Defense Force (JASDF), reducing engineering and staffing costs. In August 2009, it was reported that the F-22 would require increases to the military budget beyond the historic 1 percent of GDP. In June 2009, Japanese Defense Minister Yasukazu Hamada said Japan still sought the F-22.
Some Australian politicians and defense commentators have proposed that Australia should purchase F-22s instead of the F-35. In 2006, the Australian Labor Party supported this proposal on the grounds that the F-22 is a proven, highly capable aircraft, while the F-35 is still under development. However, Australia's Howard government ruled out purchase of the F-22, as its release for export is unlikely, and lacks sufficient ground/maritime strike capacity. The following year, the Australian government ordered a review of plans to procure the F-35 and F/A-18E/F Super Hornet, including an evaluation of the F-22's suitability. The then Defence Minister Joel Fitzgibbon stated: "I intend to pursue American politicians for access to the Raptor".In February 2008, U.S. Defense Secretary Robert Gates said he had no objection to F-22 sales to Australia.
"The IAF would be happy to equip itself with 24 F-22s, but the problem at this time is the US refusal to sell the aircraft, and its $200 million price tag."
Israeli Air Force (IAF) chief procurement officer Brigadier-General Ze'ev Snir.
Thomas Crimmins of the Washington Institute for Near East Policy speculated in 2009 that the F-22 could be a strong diplomatic tool for Israel, strengthening the capability to strike Iranian nuclear facilities. Crimmins also stated the F-22 may be the only aircraft able to evade Russian S-300 air defense systems, which Russia may sell to Iran.However, Lockheed Martin has stated that the F-35 can handle the S-300, additionally Russia has stated they support and voted for United Nations sanctions on Iran preventing sales of the S-300.
The 2010 defense authorization bill included provisions which required the DoD to prepare a report on the costs and feasibility for an F-22 export variant and another report on the impact of F-22 export sales on the U.S. aerospace industry.

Production termination

In 2006, David M. Walker, Comptroller General of the United States at the time, found that "the DOD has not demonstrated the need or value for making further investments in the F-22A program." During the two-month grounding of nearly 700 older F-15s in 2007, some US Senators demanded Deputy Secretary of Defense Gordon England release three government reports supporting additional F-22s beyond the planned 183 jets.In December 2007, the USAF requested continued production beyond the planned 183 F-22s.

Two F-22A Raptors in close trail formation
In January 2008, the Pentagon announced that it would ask Congress to fund additional F-22s to replace other aircraft lost in combat, and proposed that $497 million that would have been used to shut down the F-22 line be instead used to buy four extra F-22s, leaving the production line open beyond 2011 and allowing the next administration an option to buy more F-22s3] Funds earmarked for line shutdown were redirected to repairs upon the F-15 fleet; delaying the end of F-22 production.
On 24 September 2008, Congress passed a defense spending bill funding continued production of the F-22.On 12 November 2008, the Pentagon released $50 million of the $140 million approved by Congress to buy parts for an additional four aircraft, thus leaving the Raptor program in the hands of the incoming Obama Administration. On 6 April 2009, Secretary of Defense Gates called for the phasing out of F-22 production in fiscal year 2011, leaving the USAF with a production run of 187 fighters, minus losses. F-35 acquisition would be accelerated.On 17 June 2009 the House Armed Services Committee inserted $368.8 million in the budget towards a further 12 F-22s in FY 2011.
On 9 July 2009, General James Cartwright, Vice Chairman of the Joint Chiefs of Staff, explained to the U.S. Senate Committee on Armed Services his reasons for supporting termination of F-22 production. He stated that fifth-generation fighters need to be proliferated to all three services by shifting resources to the multirole F-35. He noted that commanders had concerns regarding electronic warfare (EW) capabilities, and that keeping the F/A-18 production line "hot" offered a fallback option to the F-35 in the EA-18G Growler.
"The Pentagon cannot continue with business as usual when it comes to the F-22 or any other program in excess of our needs."
Secretary of Defense Robert Gates, speaking on the cancellation.
On 21 July 2009, President Obama threatened to veto F-22 funding. On 21 July 2009, the Senate voted in favor of ending F-22 production. Secretary Gates said that the decision to end production was taken in light of the F-35's capabilities. On 29 July 2009, the Air National Guard's director asked for "60 to 70" F-22s for air sovereignty missions, noting that these could lack capabilities such as ground attack.On 30 July 2009, the House agreed to remove funds for an additional 12 aircraft and abide by the 187 cap. In mid-2010, Gates reduced the F-22 requirement from 243 to 187 aircraft, by lowering the preparations for two major regional conflicts to one. President Obama signed the National Defense Authorization Act for Fiscal Year 2010 in October 2009, without F-22 funding.
RAND estimated the cost of restarting production to build an additional 75 Raptors to be $17 billion or $227 million per aircraft. However Lockheed Martin has said that restarting the production line would only cost $200 millionThe RAND paper was produced as part of an USAF study to determine the costs of retaining F-22 tooling for a future Service Life Extension Program (SLEP).The tooling for F-22 production will be documented in illustrated electronic manuals stored at the Sierra Army Depot.
Russian and Chinese fighter developments have fueled concern; General John Corley, head of Air Combat Command, wrote in a 2009 letter to a senator, "In my opinion, a fleet of 187 F-22s puts execution of our current national military strategy at high risk in the near- to mid-term". But Gates replied "Nonsense". On 8 January 2011, Gates clarified that Chinese fifth-generation fighter developments had been accounted when the number of F-22s was set, and that the United States would have a considerable advantage in stealth aircraft in 2025, even with F-35 delays. On 11 January 2011, China's J-20 stealth aircraft made its first flight,leading to speculation on the reactivation of F-22 production;An August 2008 RAND study concluded the F-22 would only play a minor role in a conflict with China over Taiwan as nearby bases would be rapidly shutdown by Medium-range ballistic missiles (MRBMs); and distant bases would rely upon vulnerable aerial refueling tankers.
In December 2011, the 195th and final F-22 was completed (out of 8 test and 187 combat aircraft produced).

Upgrades

On 5 January 2001, Raptor 4005 flew with the Block 3.0 software, which was the first combat-capable avionics version. In June 2009, Increment 3.1 was tested at Edwards Air Force Base. This provided a basic ground-attack capability through Synthetic Aperture Radar mapping, Electronic attack and the GBU-39 Small Diameter Bomb. The Increment 3.1 Modification Team with the 412th Test Wing received the Chief of Staff Team Excellence Award for upgrading 149 Raptors. The fleet upgrade should start at the end of 2011.
Increment 3.2 was to add an improved SDB capability, an automatic ground collision avoidance system for low level operations and enable use of the AIM-9X Sidewinder and AIM-120D AMRAAM missiles. However, a helmet mounted cueing system has been deferred by technical issues. Increment 3.2 was expected to be fielded in FY15, possibly including the Multifunction Advanced Data Link (MADL). In July 2009 the USAF announced the modification of three business jets with the interim Battlefield Airborne Communications Node (BACN) to allow communication between F-22s and other platforms until MADL is installed.In March 2010, the USAF accelerated software portions of the Increment 3.2 upgrades to be completed in FY 2013, other upgrades will be completed later. Upgrading the first 183 aircraft to the 3.2 upgrade is estimated to cost $8 billion.In May 2009, Gen. Norton A. Schwartz and Air Force Secretary Michael B. Donley gave testimony to Congress that this would be paid for through the early retirement of legacy fighters.A total of 249 fourth-generation fighters were retired during Fiscal Year 2010. On 16 September 2009, Gates said "Our commitment to this aircraft is underscored by the 6 and-a half billion dollars... to upgrade the existing F-22 fleet to be fully mission-capable."
The USAF opened the Raptor enhancement, development and integration (FREDI) contract to other bidders in January 2011 with a total budget of $16 billion.On 18 November 2011, the upgrade contract with Lockheed Martin was increased by $1.4 billion to a maximum value of $7.4 billion. This increment opens the way for further upgrades in 2012.
Lockheed Martin has proposed upgrades to add capabilities from the newer F-35. Elements such as MADL are delayed until the F-35 program is completed to reduce risk. One upgrade from the F-35 is new high-durability stealth coatings to lower maintenance. The Ada software language was blamed for slow progress and increased costs on the program, leading to a reorganization in 2011. Increment 3.2A in 2014 focuses on electronic warfare, communications and identification. Increment 3.2B in 2017 will support the AIM-9X and AIM-120D missiles. Increment 3.2C in 2019 may migrate some avionics to an open platform, allowing features to be added by various companies. Lockheed Martin is working on upgrading the AN/AAR-56 Missile Launch Detector (MLD) to provide situational awareness and defensive Infrared Search and Track similar to the F-35's SAIRST.
The current upgrade schedule is:
  • Increment 3.1 now entering service adds capabilities for SDB, SAR, and electronic attack.
  • Update 4 in 2012 will add a rudimentary capability for the AIM-120D.
  • Increment 3.2A will be fielded in 2014 with Link 16 and electronic warfare improvements.
  • Update 5 in 2015 will add an initial capability for the AIM-9X.
  • In 2016 the fleet will be upgraded to 36 Block 20 training aircraft and 149 Block 30/35 operational aircraft.
  • Increment 3.2B in 2017 will add full capability for the air to air missiles, and improved geolocation.
  • Increment 3.2C is still being defined.
Features that are not currently planned for upgrades include:
  • Adding in the previously planned side-mounted AESA radar arrays
  • infrared search and track (IRST)
  • helmet-mounted sight
  • Powered air to surface missiles or the GBU-53 Small Diameter Bomb II in order to engage moving ground targets.
The Raptor is designed with a lifespan of 30 years and 8000 flight hours, but investigations are being made for upgrades to extend this. The F-22 is expected to eventually be replaced by the fighter from the Next Generation Air Dominance program.

Design

Characteristics

Rear view of jet aircraft in-flight at dawn/dusk above mountains. Its engines are in full afterburner, evident through the presence of shock diamonds.
F-22 Raptor flying with its F119-PW-100 engines on full afterburner
The F-22 Raptor is a fifth generation fighter that is considered a fourth-generation stealth aircraft by the USAF. Its dual afterburning Pratt & Whitney F119-PW-100 turbofans incorporate pitch axis thrust vectoring, with a range of ±20 degrees. The maximum thrust is classified, though most sources place it at about 35,000 lbf (156 kN) per engine.Maximum speed, without external weapons, is estimated to be Mach 1.82 in supercruise mode, as demonstrated by General John P. Jumper, former US Air Force Chief of Staff, when his Raptor exceeded Mach 1.7 without afterburners on 13 January 2005. With afterburners, it is "greater than Mach 2.0" (1,317 mph, 2,120 km/h). Former Lockheed chief test pilot Paul Metz stated that the Raptor has a fixed inlet, as opposed to variable intake ramps, and that the F-22 has a greater climb rate than the F-15, despite the F-15's higher thrust-to-weight ratio of 1.2:1 (the F-22 has a ratio closer to 1:1).The US Air Force claims that the Raptor cannot be matched by any known or projected fighter types,and Lockheed Martin claims: "the F-22 is the only aircraft that blends supercruise speed, super-agility, stealth and sensor fusion into a single air dominance platform."
Demonstration video of an F-22
F-22 Raptor flight demonstration video
The ability of airframes to withstand both stress and heat is a major design factor, thus the F-22 makes use of many polymers; however, as some of the materials are a significant health risk to personnel, technicians require protective equipment such as eye protection, respirators and gloves to work on the aircraft. The use of internal weapons bays allows the aircraft to maintain a comparatively higher performance while carrying a heavy payload over many other aircraft due to a lack of drag from external stores. It is one of only a few aircraft that can supercruise or sustained supersonic flight without the use of afterburners, which lowers fuel usage. The F-22 can intercept time-critical or rapidly moving targets that a subsonic aircraft would not have the speed to follow and an afterburner-dependent aircraft would lack fuel to reach.
The F-22 is highly maneuverable, at both supersonic and subsonic speeds. It is extremely departure-resistant, enabling it to remain controllable at extreme pilot inputs. The Raptor's thrust vectoring nozzles allow the aircraft to turn tightly, and perform extremely high alpha (angle of attack) maneuvers such as the Herbst maneuver (or J-turn), Pugachev's Cobra, and the Kulbit.The F-22 is also capable of maintaining a constant angle of attack of over 60°, yet still having some control of roll. During June 2006 exercises in Alaska, F-22 pilots demonstrated that cruise altitude has a significant effect on combat performance, and routinely attributed their altitude advantage as a major factor in achieving an unblemished kill ratio against other US fighters and 4th/4.5th generation fighters.
Members of the Fighter Mafia have criticized the shortcomings of the F-22 as compared to their ideal of the F-16 in pilot visibility, available flight hours for pilot training, a focus on Beyond-visual-range missile combat that ignores air combat history, stealth that does not cover important long range search frequencies, and very limited range.

Avionics

The F-22's avionics include BAE Systems E&IS radar warning receiver (RWR) AN/ALR-94, AN/AAR 56 Infra-Red and Ultra-Violet MAWS (Missile Approach Warning System) and the Northrop Grumman AN/APG-77 Active Electronically Scanned Array (AESA) radar. The AN/ALR-94 is a passive receiver system to detect radar signals; composed of more than 30 antennas blended into the wings and fuselage that provide all around coverage. It was described by Tom Burbage, former F-22 program head at Lockheed Martin, as "the most technically complex piece of equipment on the aircraft." It has a greater range (250+ nmi) than the radar, allowing the F-22 to limit its own radar emissions to maximise stealth. As a target approaches, the receiver can cue the AN/APG-77 radar to track the target with a narrow beam, which can be as focused down to 2° by 2° in azimuth and elevation.
Two personnel in white apparel handing a radar
The AN/APG-77 AESA radar
The AN/APG-77 radar, designed for air superiority and strike operations, features a low-observable, active-aperture, electronically-scanned array that can track multiple targets in any weather. The AN/APG-77 changes frequencies more than 1,000 times per second to lower interception probability. Additionally, radar emissions can be focused in an electronic-attack capability to overload enemy sensors.
The radar's information is processed by two Raytheon Common Integrated Processor (CIP)s. Each CIP can process 10.5 billion instructions per second and has 300 megabytes of memory. Information can be gathered from the radar and other onboard and offboard systems, filtered by the CIP, and offered in easy-to-digest ways on several cockpit displays, enabling the pilot to remain on top of complicated situations. The F-22s avionics software has some 1.7 million lines of code, the majority involving processing data from the radar.The radar has an estimated range of 125–150 miles, though planned upgrades will allow a range of 250 miles (400 km) or more in narrow beams. In 2007, tests by Northrop Grumman, Lockheed Martin, and L-3 Communications enabled the AESA system of a Raptor to act like a WiFi access point, able to transmit data at 548 megabits per second and receive at gigabit speed; this is far faster than the Link 16 system used by US and allied aircraft, which transfers data at just over 1 Mbit/s.
The F-22 has a threat detection and identification capability comparative with the RC-135 Rivet Joint.The F-22's stealth allows it to safely operate far closer to the battlefield, compensating for the reduced capability The F-22 is capable of functioning as a "mini-AWACS", however the radar is less powerful than dedicated platforms such as the E-3 Sentry. The F-22 allows its pilot to designate targets for cooperating F-15s and F-16s, and determine whether two friendly aircraft are targeting the same aircraft. This radar system can sometimes identify targets "many times quicker than the AWACS". The radar is capable of high-bandwidth data transmission; conventional radio "chatter" can be reduced via these alternative means.The IEEE-1394B data bus developed for the F-22 was derived from the commercial IEEE-1394 "FireWire" bus system. Sensor fusion combines data from all onboard and offboard sensors into a common view to prevent the pilot from being overwhelmed.
In a critical article former Navy Secretary John Lehman wrote "[a]t least [the F-22s] are safe from cyberattack. No one in China knows how to program the '83 vintage IBM software that runs them."[ Former Secretary of the USAF Michael Wynne blamed the use of the DoD's Ada as a reason for cost overruns and schedule slippages on many major military projects, including the F-22 Raptor. The F-22 uses the INTEGRITY-178B operating system from Green Hills Software, which is also used on the F-35, several commercial airliners and the Orion Crew Exploration Vehicle.

Cockpit


Cockpit of the F-22, showing instruments and head up display.
The F-22 uses a glass cockpit with no analog flight instruments.A side-stick controller and two throttles are the main flight controls. The stick is force sensitive and has limited movement. The cockpit interior lighting is fully night-vision goggle compatible.The monochrome head-up display by GEC (which has since become BAE Systems) offers a wide field of view and serves as a primary flight instrument for the pilot; information is also displayed upon six color liquid crystal display (LCD) panels.
The integrated control panel (ICP) is a keypad system for entering communications, navigation, and autopilot data. Two 3 × 4 in (7.6 × 10 cm) up-front displays located around the ICP are used to display integrated caution advisory/warning data, communications, navigation and identification (CNI) data[citation needed] and also serve as the stand-by flight instrumentation group and fuel quantity indicator. The stand-by flight group displays an artificial horizon, for basic instrument meteorological conditions. The 8 × 8 in (20 × 20 cm) primary multi-function display is located under the ICP, and is used for navigation and situation assessment. Three 6.25 × 6.25 in (15.9 × 15.9 cm) secondary multi-function displays are located around the PMFD for tactical information and stores management.
The canopy is approximately 140 inches long, 45 inches wide, and 27 inches tall; it lacks a canopy bow for improved vision. An iridium-tin oxide coating gives the canopy a gold color and reflects radar waves.The ejection seat is a version of the ACES II (Advanced Concept Ejection Seat) commonly used in USAF aircraft, with a center-mounted ejection control. Improvements over the previous models include an active arm restraint system to reduce injury.
The life support system integrates critical components to sustain the pilot, such as the on-board oxygen generation system (OBOGS), and a breathing regulator/anti-g valve that controls flow and pressure to the mask and garments. The pilot's protective garments are designed for chemical/biological/cold-water immersion protection, to counter g-forces and high altitudes, and provide thermal relief. The helmet incorporates active noise reduction for hearing protection.Suspicions regarding the performance of the OBOGS and life support equipment have been raised by several crashes.

Armament

Jet fighter flying above a streaking missile, which had moments earlier been released by the former.
An F-22 fires an AIM-120 AMRAAM
The Raptor has three internal weapons bays on the bottom and sides of the fuselage. It can carry six compressed carriage medium range missiles in the center bay and one short range missile in each of the two side bays. Four of the medium range missiles can be replaced with two bomb racks that can each carry one medium-size bomb or four small diameter bombs. Carrying missiles and bombs internally maintains its stealth capability and maintains lower drag resulting in higher top speeds and longer combat ranges. Launching missiles requires opening the weapons bay doors for less than a second, while the missiles are pushed clear of the airframe by hydraulic arms. This reduces the Raptor's chance of detection by enemy radar systems due to launched ordnance and also allows the F-22 to launch long range missiles while maintaining supercruise. The F-22 can also carry air-to-surface weapons such as bombs with Joint Direct Attack Munition (JDAM) guidance and the Small-Diameter Bomb, but cannot self-designate for laser-guided weapons. Air-to-surface ordnance is limited to 2,000 lb (compared to 17,000 lb of F/A-18). The Raptor has an M61A2 Vulcan 20 mm cannon in the right wing root. The M61A2 carries 480 rounds; enough ammunition for approximately five seconds of sustained fire. The opening for the cannon's firing barrel is covered by a door when not in use to maximise stealth.The F-22 has been able to close to gun range in training dogfights while avoiding detection.

For stealth, the F-22 carries weapons in internal bays. The open doors for the center bay and smaller side bays are visible here.
The Raptor's very high sustained cruise speed and operational altitude add significantly to the effective range of both air-to-air and air-to-surface munitions. This gives it a 40% greater employment range for air to air missiles than the F-35. The USAF plans to procure the AIM-120D AMRAAM, reported to have a 50% increase in range compared to the AIM-120C. While specific figures remain classified, it is expected that JDAMs employed by F-22s will have twice or more the effective range of munitions dropped by legacy platforms.In testing, a Raptor dropped a 1,000 lb (450 kg) JDAM from 50,000 feet (15,000 m), while cruising at Mach 1.5, striking a moving target 24 miles (39 km) away.
While the F-22 typically carries its weapons internally, the wings include four hardpoints, each rated to handle 5,000 lb (2,300 kg). Each hardpoint has a pylon that can carry a detachable 600 gallon fuel tank or a launcher holding two air-air missiles. However, the use of external stores has a detrimental effect on the F-22's stealth, maneuverability and speed. The two inner hardpoints are "plumbed" for external fuel tanks; the hardpoints can be jettisoned in flight so the fighter can maximise its stealth after exhausting external stores A stealth ordnance pod and pylon is being developed to carry additional weapons internally.

Stealth

The stealth of the F-22 is due to a combination of factors, including the overall shape of the aircraft, the use of radar absorbent material (RAM), and attention to detail such as hinges and pilot helmets that could provide a radar return. However, reduced radar cross section is one of five facets of presence reduction addressed in the designing of the F-22. The F-22 was designed to disguise its infrared emissions, reducing the threat of infrared homing ("heat seeking") surface-to-air or air-to-air missiles, including its flat thrust vectoring nozzles. The aircraft was designed to be less visible to the naked eye; radio, heat and noise emissions are equally controlled.
The F-22 apparently relies less on maintenance-intensive radar absorbent material and coatings than previous stealth designs like the F-117. These materials caused deployment problems due to their susceptibility to adverse weather conditions. Unlike the B-2, which requires climate-controlled hangars, the F-22 can undergo repairs on the flight line or in a normal hangar.Furthermore, the F-22 has a "Signature Assessment System", which presents warning indicators when normal wear-and-tear degrades the aircraft's radar signature to the point of requiring substantial repair work. The exact radar cross section (RCS) remains classified; however, in early 2009 Lockheed Martin released information on the F-22, indicating it to have a RCS (from certain angles) of −40 dBsm – the equivalent radar reflection of a "steel marble".Maintenance of the F-22's stealth features decreases the mission capable rate to approximately 62–70%.

F-22 with external pylons


AircraftRadar cross section (estimate)
Sukhoi Su-30MKI20 square metres
Dassault Rafale2 square metres
Eurofighter Typhoon1 square metre
Sukhoi Su-35BM1 square metre
Lockheed F-117 Nighthawk0.025 square metres
Lockheed Martin F-22 Raptor0.0001 square metres


The effectiveness of the stealth characteristics is difficult to gauge. The RCS value is a restrictive measurement of the aircraft's frontal or side area from the perspective of a static radar. As soon as the F-22 maneuvers, it exposes a completely different set of angles and surface area, increasing visibility. Furthermore, the use of stealth contouring and radar absorbent material are chiefly effective against high-frequency radars, usually found on other aircraft. Low-frequency radars, employed by weather radars and ground warning stations, are alleged to be less affected by stealth characteristics and are more capable of detecting aircraft.The result of these faint and fleeting radar contacts is that while defenders could become aware of the presence of a stealth aircraft, means of interception cannot be reliably vectored in to shoot down the aircraft.
The F-22 also includes measures designed to minimize its detection by infrared, including special paint and active cooling of leading edges to deal with the heat buildup encountered during supercruise flight.

Operational history

Designation and testing

Rear/starboard view of aerial refueling tanker transferring fuel to a jet fighter via a long boom. The two aircraft are slightly banking left.
An F-22 refuels from a KC-135 during testing; the attachment on the back top is for a spin recovery chute
The YF-22 was originally given the unofficial name "Lightning II", after the World War II fighter P-38, by Lockheed, which persisted until the mid-1990s when the USAF officially named the aircraft "Raptor". The aircraft was also briefly dubbed "SuperStar" and "Rapier". The F-35 later received the Lightning II name on 7 July 2006.In September 2002, Air Force leaders changed the Raptor's designation to F/A-22. The new designation, mimicking the Navy's F/A-18 Hornet, was intended to highlight plans for a ground-attack capability amid intense debate over the relevance of expensive air-superiority jets. The F-22 designation was reinstated on 12 December 2005, when the aircraft entered service.
Flight testing of the F-22 began in 1997. Raptor 4001 was retired and sent to Wright-Patterson AFB to be fired at for testing the fighter's survivability. Usable parts of 4001 would be used to make a new F-22. Another engineering and manufacturing development (EMD) F-22 was also retired and likely to be sent to be rebuilt. A testing aircraft was converted to a maintenance trainer at Tyndall AFB.
In May 2006, a released report documented a problem with a forward titanium boom on the aircraft. The problem was caused by a manufacturing defect in the heat-treating, making the boom less ductile than specified and potentially shortening the lives of roughly the first 80 F-22s. Modifications were implemented to restore full life expectancy.

Entering service

On 15 December 2005 the USAF announced that the Raptor had reached its Initial Operational Capability (IOC). During Exercise Northern Edge in Alaska in June 2006, 12 F-22s of the 94th FS downed 108 adversaries with no losses in simulated combat exercises.In two weeks of exercises, the Raptor-led Blue Force amassed 241 kills against two losses in air-to-air combat; neither Blue Force loss was an F-22. Shortly after was Red Flag 07-1 in February 2007. Fourteen F-22s of the 94th FS supported Blue Force strikes and undertook close air support sorties themselves. Against superior numbers of Red Force Aggressor F-15s and F-16s, 6-8 F-22s maintained air dominance throughout. No sorties were missed because of maintenance or other failures, and only one Raptor was judged lost against the opposing force's defeat. F-22s also provided airborne electronic surveillance.
Aerial port view of two aircraft in flight, one on top of the other. The bottom aircraft is a four-engined propeller-driven aircraft, which is escorted by a jet fighter. The Moon is visible as a tiny spot in the sky.
An F-22 from Elmendorf AFB, Alaska, intercepting a Russian Tupolev Tu-95 near American airspace

Deployments

While attempting its first overseas deployment to the Kadena Air Base in Okinawa, Japan, on 11 February 2007, six F-22s flying from Hickam AFB, Hawaii experienced multiple computer failures while crossing the 180th meridian of longitude (the International Date Line). The failures included navigation and communication.The fighters were able to return to Hawaii by following tanker aircraft. Within 48 hours, the error was resolved and the journey resumed. 90th Fighter Squadron performed the first F-22 NORAD interception of two Russian Tu-95MS 'Bear-H' bombers over Alaska, on 22 November 2007. Since then, F-22s have also escorted probing Tu-160 "Blackjack" strategic bombers.
On 12 December 2007, General John D.W. Corley, USAF, Commander of Air Combat Command, officially declared the F-22s of the integrated active duty 1st Fighter Wing and Virginia Air National Guard 192d Fighter Wing fully operational, three years after the first Raptor arrived at Langley Air Force Base, Virginia. This was followed from 13 to 19 April 2008 by an Operational Readiness Inspection (ORI) of the integrated wing in which it received an "excellent" rating in all categories while scoring a simulated kill-ratio of 221–0. The first pair of Raptors assigned to the 49th Fighter Wing became operational at Holloman Air Force Base, New Mexico, on 2 June 2008.
In December 2007, Secretary of the Air Force Michael Wynne requested that the F-22 be deployed to the Middle East; Secretary of Defense Gates rejected this option.Time suggested part of the reason for it not being used in the 2011 military intervention in Libya may have been its high unit cost.

An F-22 observes as an F-15 Eagle banks left. The F-22 is intended to replace the F-15C/D
On 28 August 2008, an unmodified F-22 from the 411th Flight Test Squadron performed in the first ever air-to-air refueling of an aircraft using synthetic jet fuel. The test was a part of a wider USAF effort to qualify aircraft to use the fuel, a 50/50 mix of JP-8 and a Fischer-Tropsch process-produced, natural gas-based fuel.Then in 2011 a Raptor made a supersonic flght on a 50% mixture of biofuel derived from camelina.[195]

Maintenance and training

United States Air Force video on the F-22 Raptor.
F-22 Raptor U.S. Air Force video
In 2004 the F-22 had a mission ready rate of 62% fleet wide but this was improved to 70% in 2009, with the mission ready rate being predicted to reach 85% as the fleet reached 100,000 flight hours. .
In the early years of its service, the F-22 required more than 30 hours of maintenance for every flight hour, with the total cost per flight hour of $44,000, however in 2008 this figure had been lowered to 18.1 hours, and 10.5 hours by 2009. The original Pentagon requirement was for 12hours of maintenance per flight hour, so this figure has been achieved. At introduction the F-22 also had a Mean Time Between Maintenance (MTBM) of 1.7 hours, however in the 7 years since this has been improved to 3.2 hours, exceeding the original Pentagon requirement of 3.0 hours by 2010.
Each Raptor requires a month-long packaged maintenance plan (PMP) after every 300 flight hours. The aircraft's stealth system, including its radar absorbing metallic skin, account for almost one third of all maintenance. Another source of maintenance problems is that many components require custom hand-fitting and are not interchangeable. The canopy of the aircraft was required to have a life of 800 hours, however the original design failed to meet this, averaging at 331 hours. In response to this the canopy was redesigned, and the new canopy has met its requirements of a 800 hour life expectancy.
In January 2007, it was reported that the F-22 maintained a 97% sortie rate (flying 102 out of 105 tasked sorties) while amassing a 144-to-zero kill ratio during "Northern Edge" air-to-air exercises held in Alaska, the first large-scale exercise in which the Raptor participated. Lt. Col. Wade Tolliver, the squadron commander of the 27th FS commented: "the stealth coatings are not as fragile as they were in earlier stealth aircraft. It isn't damaged by a rain storm and it can stand the wear and tear of combat without degradation."However, rain has caused "shorts and failures in sophisticated electrical components" when the Raptors were briefly posted to Guam.
In its 2012 budget request the USAF cut F-22 flight training hours by one-third to reduce the operating costs of flying the aircraft. The F-22 will continue in its role as an airshow demonstration aircraft and will be the only USAF solo aircraft demonstrator in 2012.

Operational problems

During 2010–2011 periodic operational hazards surfaced regarding F-22 operations. In February 2010 the entire fleet was grounded due to rusting ejection seat rods.In May 2011 the entire fleet was grounded; following the November 2010 crash near Elmendorf Air Force Base, Alaska the F-22 had been restricted to flying below 25,000 feet while the Honeywell oxygen generating system was inspected. After five incidents of pilots suffering from hypoxia and decompression, General William M. Fraser III of Air Combat Command grounded the F-22 fleet indefinitely on 3 May 2011. In June 2011, the investigation broadened across the life support systems,and aircraft deliveries were stopped.
In July 2011 the investigation suspected a scenario in which the pilots were poisoned by carbon monoxide from the engines while warming up the plane inside the hangars.Tests on pilots have found other chemicals have been inhaled from the on-board oxygen generating system (OBOGS), including oil fumes and propane
In September 2011, the F-22 returned to flight with added pilot safety equipment and careful monitoring of crew and aircraft, while the investigation continued. On 21 October 2011, Langley's F-22s were grounded after a suspected oxygen system problem; Elmendorf-Richardson grounded their aircraft as well.All aircraft were cleared to fly again on October 25.In late October 2011, Lockheed Martin was awarded a $24M contract to find the cause of the oxygen system difficulty, as well as providing other sustainment functions. In mid-December 2011, the Air Force said that there had been 14 episodes since September, when the planes returned to operation, in which pilots experienced "physiological incidents" which might have been caused by a lack of oxygen. A USAF report released on 13 January 2012 stated that toxins entering the aircraft environmental control system and associated onboard oxygen generation system caused the hypoxia-like symptoms in pilots and aircraft maintenance personnel between April and September 2011. The report did not conclusively indentify the cause for the problem.

Variants

  • YF-22A – pre-production version used for ATF testing and evaluation. Two were built.
  • F-22A – single-seat production version. Was designated "F/A-22A" in early 2000s.
  • F-22B – planned two-seat variant, but was dropped in 1996 to save development costs.
  • Naval F-22 variant – a carrier-borne variant of the F-22 with swing-wings for the U.S. Navy's Navy Advanced Tactical Fighter (NATF) program to replace the F-14 Tomcat. Program was canceled in 1993.
Derivatives
The FB-22 was a proposed medium-range bomber for the USAF.The FB-22 was projected to carry up to 30 Small Diameter Bombs to about twice the range of the F-22A, while maintaining the F-22's stealth and supersonic speed. However, the FB-22 in its planned form appears to have been canceled with the 2006 Quadrennial Defense Review and subsequent developments, in lieu of a larger subsonic bomber with a much greater range.
The X-44 MANTA, or multi-axis, no-tail aircraft, was a planned experimental aircraft based on the F-22 with enhanced thrust vectoring controls and no aerodynamic backup. The aircraft was to be solely controlled by thrust vectoring, without featuring any rudders, ailerons, or elevators. Funding for this program was halted in 2000.

 


F-22A Raptor from Tyndall AFB, Florida cruising over the Florida Panhandle

An F-22 landing at Holloman AFB, New Mexico

An F-22, based at Elmendorf AFB, Alaska, over mountain terrain


 Notable accidents

Because of the platform's relative immaturity due to its early operational status and low number of flight hours compared to other platforms, the F-22 has the highest accident rate of any USAF fighter aircraft in service. This rate is expected to go down as the Air Force gains more experience in operating the aircraft.
In April 1992, the first YF-22 crashed while landing at Edwards Air Force Base, California. The test pilot Tom Morgenfeld escaped without injury. The cause of the crash was found to be a flight control software error that failed to prevent a pilot-induced oscillation.
The first crash of a production F-22 occurred during takeoff at Nellis Air Force Base on 20 December 2004, in which the pilot ejected safely before impact. The crash investigation revealed that a brief interruption in power during an engine shutdown prior to flight caused a malfunction in the flight-control system; consequently the aircraft design was corrected to avoid the problem. All F-22s were grounded after the crash; operations resumed following a review.
On 25 March 2009, an F-22 crashed 35 miles (56 km) northeast of Edwards Air Force Base during a test flight, resulting in the death of Lockheed test pilot David P. Cooley. An Air Force Materiel Command investigation found that Cooley momentarily lost consciousness during a high-G maneuver, then ejected when he found himself too low to recover. Cooley was killed during ejection by blunt-force trauma from the aircraft's speed and the windblast. The investigation found no issues with the F-22's design.
On 16 November 2010, an F-22, based at Elmendorf, Alaska, lost contact with Air Traffic Control. The aircraft was discovered to have crashed; the pilot, Captain Jeffrey Haney, did not survive. The F-22 fleet was restricted to flying below 25,000 feet, before being grounded completely, while the accident was investigated. During the summer of 2011, more wreckage from the crash site was recovered; the accident has been attributed to a malfunction in the bleed air system that shut down the aircraft's Environmental Control System (ECS) and On-Board Oxygen Generating System (OBOGS). The OBOGS was apparently shut down automatically in response to an overheat condition detected by the main computer.The accident review board, however, ruled the pilot was to blame for the accident, as he did not react properly and did not engage the emergency oxygen system.

Aircraft on display

In April 2007 The National Museum of the United States Air Force announced it had added EMD F-22A 91-4003 to its collection. It would later be put on display in the space being occupied by a YF-22. The Museum publicly unveiled its F-22 display on 18 January 2008.

Specifications

Orthographically projected diagram of the F-22A

F-22 with drop tanks in transit to Kadena Air Base, Japan from Langley Air Force Base, Virginia
Data from USAF,F-22 Raptor Team web site, Lockheed Martin, Aviation Week, Journal of Electronic Defense, and Manufacturers' data
General characteristics
  • Crew: 1
  • Length: 62 ft 1 in (18.90 m)
  • Wingspan: 44 ft 6 in (13.56 m)
  • Height: 16 ft 8 in (5.08 m)
  • Wing area: 840 ft² (78.04 m²)
  • Airfoil: NACA 64A?05.92 root, NACA 64A?04.29 tip
  • Empty weight: 43,430 lb (19,700 kg)
  • Loaded weight: 64,460 lb (29,300 kg)
  • Max. takeoff weight: 83,500 lb (38,000 kg)
  • Powerplant: 2 × Pratt & Whitney F119-PW-100 Pitch Thrust vectoring turbofans
    • Dry thrust: 23,500 lb(104 kN) each
    • Thrust with afterburner: 35,000+ lb(156+ kN) each
  • Fuel capacity: 18,000 lb (8,200 kg) internally, or 26,000 lb (11,900 kg) with two external fuel tanks

Performance
  • Maximum speed:
    • At altitude: Mach 2.25 (1,500 mph, 2,410 km/h) [estimated]
    • Supercruise: Mach 1.82 (1,220 mph, 1,963 km/h)
  • Range: >1,600 nmi (1,840 mi, 2,960 km) with 2 external fuel tanks
  • Combat radius: 410 nmi (with 100 nmi in supercruise) (471 mi, 759 km)
  • Ferry range: 2,000 mi (1,738 nmi, 3,219 km)
  • Service ceiling: 65,000 ft (19,812 m)
  • Wing loading: 77 lb/ft² (375 kg/m²)
  • Thrust/weight: 1.09 (1.26 with loaded weight & 50% fuel)
  • Maximum design g-load: -3.0/+9.0 g

USAF poster overview of key features and armament
Armament
  • Guns: 1× 20 mm (0.787 in) M61A2 Vulcan 6-barreled gatling cannon in starboard wing root, 480 rounds
  • Air to air loadout:
    • 6× AIM-120 AMRAAM
    • 2× AIM-9 Sidewinder
  • Air to ground loadout:
    • 2× AIM-120 AMRAAM and
    • 2× AIM-9 Sidewinder for self-protection, and one of the following:
      • 2× 1,000 lb (450 kg) JDAM or
      • 8× 250 lb (110 kg) GBU-39 Small Diameter Bombs
  • Hardpoints: 4× under-wing pylon stations can be fitted to carry 600 US gallon drop tanks or weapons, each with a capacity of 5,000 lb (2,268 kg).
Avionics
  • RWR (Radar warning receiver): 250 nmi (463 km) or more
  • Radar: 125–150 miles (200–240 km) against 1 m2 (11 sq ft) targets (estimated range)
  • Chemring MJU-39/40 flares for protection against IR missiles.