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Another program that the Air Force is considering is the "Avionics Modernization Program" (AMP). AMP would equip the E-3s with [[glass cockpit]]s. The Air Force also wants modified E-3s with jet engines that are more reliable than the original ones, and also with at least 19% higher fuel efficiencies. New turbofan engines would give these E-3s longer ranges, longer time-on-station, and a shorter critical runway length. If the modification is carried out, the E-3s could take off with full fuel loads using runways only {{convert|10000|ft|m|abbr=on}} long, and also at higher [[ambient temperature]]s and lower [[barometric pressure]]s, such as from bases in mountainous areas. The [[E-8 Joint STARS]] briefly fitted a test aircraft with the new [[Pratt & Whitney JT8D|Pratt & Whitney JT8D-219]] turbofans, stated as having one-half the cost of the competing engine, the [[CFM International CFM56|CFM56]], the Air Force is again studying the possibility of replacing the E-3's original turbofan engines with more-efficient ones.<ref>{{Cite news|url=http://www.highbeam.com/doc/1G1-76547425.html|archive-url=https://web.archive.org/web/20121106062854/http://www.highbeam.com/doc/1G1-76547425.html|url-status=dead|archive-date=6 November 2012|title=EADS, Northrop Grumman, Partt and Whitney To Offer NATO AWACS Upgrade|work=Defense Daily International|date=13 July 2001|accessdate=8 September 2010}}</ref>
Another program that the Air Force is considering is the "Avionics Modernization Program" (AMP). AMP would equip the E-3s with [[glass cockpit]]s. The Air Force also wants modified E-3s with jet engines that are more reliable than the original ones, and also with at least 19% higher fuel efficiencies. New turbofan engines would give these E-3s longer ranges, longer time-on-station, and a shorter critical runway length. If the modification is carried out, the E-3s could take off with full fuel loads using runways only {{convert|10000|ft|m|abbr=on}} long, and also at higher [[ambient temperature]]s and lower [[barometric pressure]]s, such as from bases in mountainous areas. The [[E-8 Joint STARS]] briefly fitted a test aircraft with the new [[Pratt & Whitney JT8D|Pratt & Whitney JT8D-219]] turbofans, stated as having one-half the cost of the competing engine, the [[CFM International CFM56|CFM56]], the Air Force is again studying the possibility of replacing the E-3's original turbofan engines with more-efficient ones.<ref>{{Cite news|url=http://www.highbeam.com/doc/1G1-76547425.html|archive-url=https://web.archive.org/web/20121106062854/http://www.highbeam.com/doc/1G1-76547425.html|url-status=dead|archive-date=6 November 2012|title=EADS, Northrop Grumman, Partt and Whitney To Offer NATO AWACS Upgrade|work=Defense Daily International|date=13 July 2001|accessdate=8 September 2010}}</ref>


NATO intends to extend the operational status of its AWACS until 2035.<ref>NATO summit Warsaw July 2016</ref> To comply 14 AWACS aircraft will be significantly modified in the ''Final Lifetime Extension Program'' (FLEP). Most FLEP modifications will be implemented in the communications and operational systems area e.g. expansion of data capacity, expansion of bandwidth for satellite communications, new encryption equipment, new ''have quick'' radios, upgraded mission computing hard- and software and new operator consoles. The supporting groundsystems (mission training center and mission planning and evaluation system) will also be upgraded to the latest configuration. NATO Airborne Early Warning & Control Program Management Agency (NAPMA) is the preparing and executing authority for the FLEP which will be implemented from 2019–2026. To minimize impact on the operational capacity the NAEW&C force commander will be informed in advance. FLEP will be combined with the standard planned higher echelon technical mainenance.
NATO intends to extend the operational status of its AWACS until 2035.<ref>NATO summit Warsaw July 2016</ref> To comply, fourteen AWACS aircraft will be significantly modified in the ''Final Lifetime Extension Program'' (FLEP). Most FLEP modifications will be implemented in the communications and operational systems area e.g. expansion of data capacity, expansion of bandwidth for satellite communications, new encryption equipment, new ''have quick'' radios, upgraded mission computing hard- and software and new operator consoles. The supporting groundsystems (mission training center and mission planning and evaluation system) will also be upgraded to the latest configuration. NATO Airborne Early Warning & Control Program Management Agency (NAPMA) is the preparing and executing authority for the FLEP which will be implemented from 2019–2026. To minimize impact on the operational capacity the NAEW&C force commander will be informed in advance. FLEP will be combined with the standard planned higher echelon technical mainenance.


==Design==
==Design==

Revision as of 18:12, 11 October 2019

E-3 Sentry
Aerial view port view of white jet aircraft in-flight. It has a large disc-like black radar lying horizontally above two convergent struts.
An E-3 Sentry of the United States Air Force
Role Airborne early warning and control (AEW&C)
National origin United States
Manufacturer Boeing Defense, Space & Security
Westinghouse Electric (radar)
First flight EC-137D: 9 February 1972
E-3: 25 May 1976[N 1]
Introduction March 1977
Status Operational
Primary users United States Air Force
NATO
Royal Air Force
Royal Saudi Air Force
Produced 1977–1992
Number built 68
Developed from Boeing 707

The Boeing E-3 Sentry, commonly known as AWACS, is an American airborne early warning and control (AEW&C) aircraft developed by Boeing. Derived from the Boeing 707, it provides all-weather surveillance, command, control, and communications, and is used by the United States Air Force, NATO, Royal Air Force, French Air Force, and Royal Saudi Air Force. The E-3 is distinguished by the distinctive rotating radar dome (ROTODOME) above the fuselage. Production ended in 1992 after 68 aircraft had been built.

In the mid-1960s, the US Air Force (USAF) was seeking an aircraft to replace its piston-engined Lockheed EC-121 Warning Star, which had been in service for over a decade. After issuing preliminary development contracts to three companies, the USAF picked Boeing to construct two airframes to test Westinghouse Electric and Hughes's competing radars. Both radars used pulse-Doppler technology, with Westinghouse's design emerging as the contract winner. Testing on the first production E-3 began in October 1975.

The first USAF E-3 was delivered in March 1977, and during the next seven years, a total of 34 aircraft were manufactured. NATO, as a single identity, also had 18 aircraft manufactured, basing them in Germany. The E-3 was also sold to the United Kingdom (seven) and France (four) and Saudi Arabia (five, plus eight E-3-derived tanker aircraft). In 1991, when the last aircraft had been delivered, E-3s participated in Operation Desert Storm, playing a crucial role of directing coalition aircraft against the enemy. Throughout the aircraft's service life, numerous upgrades were performed to enhance its capabilities. In 1996, Westinghouse Electric's Defense & Electronic Systems division was acquired by Northrop Corporation, before being renamed Northrop Grumman Mission Systems, which currently supports the E-3's radar.

Development

Background

In 1963, the USAF asked for proposals for an Airborne Warning and Control System (AWACS) to replace its EC-121 Warning Stars, which had served in the airborne early warning role for over a decade.[2] The new aircraft would take advantage of improvements in radar technology and in computer aided radar data analysis and data reduction. These developments allowed airborne radars to "look down", detect the movement of low-flying aircraft (see Look-down/shoot-down), and discriminate, even over land, target aircraft's movements—previously this had been impossible, due to the inability to discriminate an aircraft's track from ground clutter.[3] Contracts were issued to Boeing, Douglas, and Lockheed, the latter being eliminated in July 1966. In 1967, a parallel program was put into place to develop the radar, with Westinghouse Electric and Hughes Aircraft being asked to compete in producing the radar system. In 1968, it was referred to as Overland Radar Technology (ORT) during development tests on the modified EC-121Q.[4][5] The Westinghouse radar antenna was going to be used by whichever company won the radar competition, since Westinghouse had pioneered in the design of high-power RF phase-shifters, which are used to both focus the RF into a pencil beam, and scan electronically for altitude determination.

Black-and-white photograph of piston-engined aircraft with a large hump on midfuselage
The piston-engined EC-121 Warning Star, military version of the Lockheed Constellation, saw service in the mid-1950s.

Boeing initially proposed a purpose-built aircraft, but tests indicated it would not outperform the already-operational 707, so the latter was chosen instead. To increase endurance, this design was to be powered by eight General Electric TF34s. It would carry its radar in a rotating dome mounted at the top of a forward-swept tail, above the fuselage.[3][6] Boeing was selected ahead of McDonnell Douglas's DC-8-based proposal in July 1970. Initial orders were placed for two aircraft, designated EC-137D as test beds to evaluate the two competing radars. As the test-beds did not need the same 14-hour endurance demanded of the production aircraft, the EC-137s retained the Pratt & Whitney JT3D commercial engines, and a later reduction in endurance requirement led to retaining the normal engines in production.[5]

The first EC-137 made its maiden flight on 9 February 1972, with the fly-off between the two radars taking place during March–July that year.[4] Favorable test results led to the selection of Westinghouse's radar for the production aircraft.[7] Hughes's radar was initially thought to be a certain winner, simply because much of its design was also going into the new F-15 Eagle's radar program. The Westinghouse radar used a pipelined fast Fourier transform (FFT) to digitally resolve 128 Doppler frequencies, while Hughes's radars used analog filters based on the design for the F-15 fighter. Westinghouse's engineering team won this competition by using a programmable 18-bit computer whose software could be modified before each mission. This computer was the AN/AYK-8 design from the B-57G program, and designated AYK-8-EP1 for its much expanded memory. This radar also multiplexed a beyond-the-horizon (BTH) pulse mode that could complement the pulse-Doppler radar mode. This proved to be beneficial especially when the BTH mode is used to detect ships at sea when the radar beam is directed below the horizon.[8]

Full-scale development

Approval was given on 26 January 1973 for full-scale development of the AWACS system. To allow further development of the aircraft's systems, orders were placed for three preproduction aircraft, the first of which performed its maiden flight in February 1975. To save costs, the endurance requirements were relaxed, allowing the new aircraft to retain the four JT3D (U.S. military designation TF33) engines.[5][9] IBM and Hazeltine were selected to develop the mission computer and display system. The IBM computer was designated 4PI, and the software was written in JOVIAL. A Semi-Automatic Ground Environment (SAGE) or back-up interceptor control (BUIC) operator would immediately be at home with the track displays and tabular displays, but differences in symbology would create compatibility problems in tactical ground radar systems in Iceland, mainland Europe, and South Korea over Link-11 (TADIL-A).

Black-and-white photograph with angled front view of four-engine jet aircraft on ramp with front fuselage door opened: A contingent of people are there to welcome the jet, which has a disc-shaped radar perching on top of struts on the dorsal fuselage.
Welcome ceremony for first E-3 aircraft at Tinker AFB in 1977

Modifications to the Boeing 707 for the E-3 Sentry included a rotating radar dome (rotodome), uprated hydraulics from 241 to 345 bar (3500 - 5000 PSI) to drive the rotodome,[10] single-point ground refueling, air refueling, and a bail-out tunnel or chute. The original design had two (one forward, and one aft), but the aft bail-out chute was deleted to cut mounting costs.[11] Engineering, test and evaluation began on the first E-3 Sentry in October 1975. Between 1977 and 1992, a total of 68 E-3s were built.[12][13]

Future status

Because the Boeing 707 is no longer in production, the E-3 mission package has been fitted into the Boeing E-767 for the Japan Air Self Defense Forces. The E-10 MC2A was intended to replace USAF E-3s—along with the RC-135 and the E-8, but the E-10 program was canceled by the Department of Defense. The USAF is now performing a series of incremental improvements, mainly to avionics, to bring the E-3 up to current standards of performance. Boeing is flight-testing its Block 40/45 E-3s. This modified E-3 contains upgrades of the mission crew and air battle management sections, as well as significantly upgraded electronic equipment.[14]

Another program that the Air Force is considering is the "Avionics Modernization Program" (AMP). AMP would equip the E-3s with glass cockpits. The Air Force also wants modified E-3s with jet engines that are more reliable than the original ones, and also with at least 19% higher fuel efficiencies. New turbofan engines would give these E-3s longer ranges, longer time-on-station, and a shorter critical runway length. If the modification is carried out, the E-3s could take off with full fuel loads using runways only 10,000 ft (3,000 m) long, and also at higher ambient temperatures and lower barometric pressures, such as from bases in mountainous areas. The E-8 Joint STARS briefly fitted a test aircraft with the new Pratt & Whitney JT8D-219 turbofans, stated as having one-half the cost of the competing engine, the CFM56, the Air Force is again studying the possibility of replacing the E-3's original turbofan engines with more-efficient ones.[15]

NATO intends to extend the operational status of its AWACS until 2035.[16] To comply, fourteen AWACS aircraft will be significantly modified in the Final Lifetime Extension Program (FLEP). Most FLEP modifications will be implemented in the communications and operational systems area e.g. expansion of data capacity, expansion of bandwidth for satellite communications, new encryption equipment, new have quick radios, upgraded mission computing hard- and software and new operator consoles. The supporting groundsystems (mission training center and mission planning and evaluation system) will also be upgraded to the latest configuration. NATO Airborne Early Warning & Control Program Management Agency (NAPMA) is the preparing and executing authority for the FLEP which will be implemented from 2019–2026. To minimize impact on the operational capacity the NAEW&C force commander will be informed in advance. FLEP will be combined with the standard planned higher echelon technical mainenance.

Design

Overview

See also: Boeing 707 – Design

The E-3 Sentry's airframe is a modified Boeing 707-320B Advanced model. USAF and NATO E-3s have an unrefueled range of some 4,000 mi (6,400 km) or eight hours of flying.[17] The newer E-3 versions bought by France, Saudi Arabia, and the UK are equipped with newer CFM56-2 turbofan engines, and these can fly for about 11 hours or about 5,000 mi (8,000 km).[18] The Sentry's range and on-station time can be increased through air-to-air refueling and the crews can work in shifts by the use of an on-board crew rest and meals area. The aircraft are equipped with one toilet in the rear, and a urinal behind the cockpit. The Saudi E-3 was delivered with an additional toilet in the rear.[12][13]

When deployed, the E-3 monitors an assigned area of the battlefield and provides information for commanders of air operations to gain and maintain control of the battle; while as an air defense asset, E-3s can detect, identify, and track airborne enemy forces far from the boundaries of the U.S. or NATO countries and can direct fighter-interceptor aircraft to these targets.[12] In support of air-to-ground operations, the E-3 can provide direct information needed for interdiction, reconnaissance, airlift, and close-air support for friendly ground forces.[12]

Avionics

AN/APY-1 [uk] antenna array in the National Electronics Museum

The unpressurized rotodome is 30 feet (9.1 m) in diameter, 6 feet (1.8 m) thick at the center, and is held 11 feet (3.4 m) above the fuselage by 2 struts.[12] It is tilted down at the front to reduce its aerodynamic drag, which lessens its detrimental effect on take-offs and endurance (which is corrected electronically by both the radar and secondary surveillance radar antenna phase shifters). The rotodome uses bleed air, outside cooling doors, and fluorocarbon based cold plate cooling to maintain the electronic and mechanical equipment temperatures. The hydraulically rotated antenna system permits the Westinghouse Corporation's AN/APY-1 [uk] and AN/APY-2 passive electronically scanned array radar system[19] to provide surveillance from the Earth's surface up into the stratosphere, over land or water.

Air Controllers aboard during Operation Provide Comfort
Close-up view of black disc-shaped radar with wide diagonal white band. The radar rests on 2 convergent struts above aircraft fuselage.
Close-up rotodome revolving at 6 revolutions per minute.[20]

Other major subsystems in the E-3 Sentry are navigation, communications, and computers. 14 consoles display computer-processed data in graphic and tabular format on screens. Its operators perform surveillance, identification, weapons control, battle management and communications functions.[12] The E-3's radar and computer subsystems gather and present broad and detailed battlefield information including position and tracking information of enemy aircraft and vessels, and of course location and status of all friendly assets. Data may be forwarded in real-time to any major command and control center in rear areas or aboard ships. In times of crisis, data may also be forwarded to the National Command Authority in the U.S. via RC-135 or naval aircraft carrier task forces.[12]

Electrical generators mounted in each of the E-3's 4r engines provide 1 megawatt of electrical power required by the E-3's radars and electronics.[12] Its pulse-Doppler radar (PD) has a range of more than 250 mi (400 km) for low-flying targets at its operating altitude, and the pulse (BTH) radar has a range of approximately 400 mi (650 km) for aircraft flying at medium to high altitudes. The radar, combined with a secondary surveillance radar (SSR) and electronic support measures (ESM), provides a look down capability, to detect, identify, and track low-flying aircraft, while eliminating ground clutter (radar) returns.[12][13][21]

Upgrades

Inside military aircraft. Two personnel wearing green clothes and blue gloves manning communications consoles with wide displays.
The command & comms consoles.

Starting in 1987, USAF E-3s were upgraded under the "Block 30/35 Modification Program" to enhance the E-3's capabilities. On 30 October 2001, the final airframe to be upgraded under this program was rolled out.[22] Several major enhancements were made, firstly the installation of ESM and an electronic surveillance capability, for both active and passive means of detection. Also, Joint Tactical Information Distribution System (JTIDS) was installed, which provides rapid and secure communication for transmitting information, including target positions and identification data, to other friendly platforms. Global Positioning System (GPS) capability was also added. Onboard computers were also overhauled to accommodate JTIDS, Link-16, the new ESM systems and to provide for future enhancements.[22]

The Radar System Improvement Program (RSIP) was a joint US/NATO development program.[12] RSIP enhances the operational capability of the E-3 radars' electronic countermeasures, and dramatically improve the system's reliability, maintainability, and availability.[12] Essentially, this program replaced the older transistor-transistor logic (TTL) and emitter-coupled logic (MECL) electronic components, long-since out of production, with off-the-shelf digital computers that utilised a High-level programming language instead of assembly language. Significant improvement came from adding pulse compression to the pulse-Doppler mode, replacing the old 8-bit FFT with 24-bit FFTs, and the 12-bit A/D (Sign + 12-bits) with a 15-bit A/D (Sign + 15-bits).[8] These hardware and software modifications improve the E-3 radars' performance, providing enhanced detection with an emphasis towards low radar cross-section (RCS) targets.[12]

The RAF had also joined the USAF in adding RSIP to upgrade the E-3's radars. The retrofitting of the E-3 squadrons was completed in December 2000. Along with the RSIP upgrade was installation of the Global Positioning System/Inertial Navigation Systems which dramatically improve positioning accuracy. In 2002, Boeing was awarded a contract to add RSIP to the small French AWACS squadron. Installation was completed in 2006.[12][23]

In the 1990s all NATO AWACS aircraft have been upgraded by the Radar System Improvement System (RSIP), a US/NATO joint venture in the area of hard and software modifications of the existing radarsystem. This resulted in an aircraft with 2 large sensorpods alongside the fuselage and a 'bulb' under the aircraft nose containing the electronic warfare equipment.[24]

After several years of planning in 2000 NATO decided to bring the E-3's on Mid Term Program (MTP) standard. Again this implied technical upgrades and a total multi-sensor-systems integration. MTP ended in 2008.

In 2009, the USAF, in cooperation with NATO, entered into a major flight deck avionics modernization program in order to maintain compliance with worldwide airspace mandates. The program, called DRAGON (for DMS Replacement of Avionics for Global Operation and Navigation), was awarded in 2010 – the prime was Boeing and the subcontractor was Rockwell Collins. Drawing on their Flight2 Flight Management System (FMS), almost all the existing avionics were replaced with new, more modern digital equipment from Rockwell Collins. The major upgraded capabilities include a Digital Audio Distribution System, Mode-5/ADS-B transponder, Inmarsat & VDL datalinks, and a Terrain Avoidance and Warning System (TAWS). The navigation system is capable of RNP-0.3, STARs and LNAV/VNAV approaches, and SIDs. The centerpiece flight deck hardware consists of five 6x8 color graphics displays (2 PFDs, 2 IMFDs, and an EICAS), two color CDUs, and a Thales ISD standby. DRAGON lays the foundation for subsequent upgrades including GPS M-Code, Iridium ATC, and Autopilot. USAF DRAGON Production begins in 2018.[25]

Operational history

Four-engined jet aircraft in-flight with landing gear partially extended. A large disc-shaped radar perches on two convergent struts on the aft fuselage.
NATO E-3s with LX tail registration,[26] as they are registered with Luxembourg. The chin bulge house a suite of electronic warfare support measures.[26]
Four-engined jet aircraft with disc-shaped radar on fuselage in-flight flanked by two jet fighters.
RAF E-3D Sentry AEW1 accompanied by Panavia Tornado F3s at Kemble Air Day. RAF AEW1s have electronic support measures pods on the wingtips.[26]

In March 1977, the 552nd Airborne Warning and Control Wing (now the 552d Air Control Wing) at Tinker AFB, Oklahoma received the first E-3 aircraft, flown and commanded by Major James R. Sterk.[12] The 34th and last USAF Sentry was delivered in June 1984.[27] In March 1996, the USAF activated the 513th Air Control Group (513 ACG), an ACC-gained Air Force Reserve Command (AFRC) AWACS unit under the Reserve Associate Program. Collocated with the 552 ACW at Tinker AFB, the 513 ACG which performs similar duties on active duty E-3 aircraft shared with the 552 ACW.[12]

The USAF has a total of thirty-one E-3s in active service. Twenty-seven are stationed at Tinker AFB and belong to the Air Combat Command (ACC). Four are assigned to the Pacific Air Forces (PACAF) and stationed at Kadena AB, Okinawa and Elmendorf AFB, Alaska. One aircraft (TS-3) was assigned to Boeing for testing and development (retired/scrapped June 2012).[12]

In 1977, Iran placed an order for ten E-3s, however this order was cancelled following the 1979 overthrow of the Iranian government.

NATO acquired 18 E-3As and support equipment for a NATO air defense force. Since all aircraft must be registered with a certain country, the decision was made to register the 18 NATO Sentries with Luxembourg, a NATO member that previously did not have any air force. The first NATO E-3 was delivered in January 1982.[26] The eighteen E-3s were operated by Number 1, 2 and 3 Squadrons of NATO's E-3 Component, based at NATO Air Base Geilenkirchen.[26] Presently, 16 NATO E-3As are in the inventory, since one E-3 was lost in a crash and one was retired from service in 2015.[27][28]

NATO's E-3A's played a very important role in the air campaign against Serbia and Montenegro in the former republic of Yugoslavia. From March – June 1999 the aircraft have been deployed in operation Allied Force directing allied strike and air defence aircraft to and from their targets.[29] Over 1.000 aircraft operating from bases in Germany and Italy took part in the air campaign which was designed to destroy Yugoslav air defenses and high-value targets such as bridges across the Danube, factories, powerstations, telecommunications facilities, military installations and the Avala TV Tower.

The United Kingdom and France are not part of the NATO E-3A Component, instead procuring E-3 aircraft through a joint project.[30] The UK and France operate their E-3 aircraft independently of each other and of NATO.[31] The UK operates six aircraft (with a seventh now retired)[32] and France operates four aircraft, all fitted with the newer CFM56-2 engines.[13] The British requirement came about following the cancellation of the British Aerospace Nimrod AEW3 project to replace the Avro Shackleton AEW2 during the 1980s. The UK E-3 order was placed in February 1987, with deliveries starting in 1990.[23][33] The other operator of the type, delivered between June 1986 and September 1987, is Saudi Arabia which operates five aircraft, all fitted with CFM56-2 engines.[13] This particular sale was hotly contested between the Reagan administration and opponents of the sale, mainly the Israeli lobby in the United States and their allies in Congress. [citation needed]

E-3 Sentry aircraft were among the first to deploy during Operation Desert Shield, where they immediately established as an around-the-clock radar screen to defend against Iraqi forces. During Operation Desert Storm, E-3s flew 379 missions and logged 5,052 hours of on-station time.[34] The data collection capability of the E-3 radar and computer subsystems allowed an entire air war to be recorded for the first time in history. In addition to providing senior leadership with time-critical information on the actions of enemy forces, E-3 controllers assisted in 38 of the 41 air-to-air kills recorded during the conflict.[12][34]

NATO E-3s joined their USAF colleagues for joint air defense as part of Operation Eagle Assist in the wake of the September 11, 2001 terrorist attacks on the World Trade Center towers and the Pentagon.[35]

NATO and RAF E-3s participated in the international military operation in Libya.[36]

On 27 January 2015, the RAF deployed an E-3D Sentry to Cyprus in support of U.S.-led coalition airstrikes against Islamic State militants in Iraq and Syria. The Sentry joins RAF Panavia Tornado, MQ-9 Reaper, and AirTanker Voyager aircraft performing or supporting almost daily strikes against militants.[37]

On 23 June 2015, the first of the original 18 NATO E-3A AWACS aircraft to retire, arrived at Davis-Monthan AFB near Tucson, AZ. The aircraft, LX-N 90449, will be placed in parts reclamation storage where critical parts will be removed by NATO technicians to support their remaining fleet of 16 Boeing E-3A aircraft. It had accumulated 22,206 flight hours between 19 August 1983 and 13 May 2015 and operated out of twenty-one different countries in support of NATO operational activities. The aircraft was due in mid-July 2015 for a six-year cycle Depot Level Maintenance (DLM) inspection which would have been very costly. Without the inspection, the aircraft would no longer be allowed to fly. The so-called "449 Retirement Project" will result in reclamation of critical parts with a value of upwards of $40,000,000. Some of the parts to be removed are no longer on the market or have become very expensive.[38][39]

On 18 November 2015, an E-3G was deployed to the Middle East to begin "immediately" flying combat missions in support of Operation Inherent Resolve against ISIL, marking the first combat deployment of the upgraded AWACS Block 40/45. The $2.7 billion development effort started in 2003, with the first five aircraft achieving initial operational capability (IOC) in July 2015. The Block 40/45 upgrade is the most extensive the E-3 has undergone, replacing its 1970s computer technology with an early 2000s standard and including a deployable ground system that receives, processes, and disseminates data. The Air Force plans to convert 24 AWACS to E-3G standard, while retiring seven from the fleet to avoid upgrade costs and harvest out-of-production components.[40]

Variants

EC-137D
2 prototype AWACS aircraft with JT3D engines, 1 fitted with a Westinghouse Electric radar and 1 with a Hughes Aircraft Company radar. Both converted to E-3A standard with TF33 engines.
E-3A
Production aircraft with TF33 engines and AN/APY-1 radar, 24 built for USAF (later converted to E-3B standard), total of 34 ordered but the last 9 completed as E-3C.[41] One additional aircraft retained by Boeing for testing,[41] 18 built for NATO with TF33 engines and 5 for Saudi Arabia with CFM56 engines.[41]
KE-3A
These are no AWACS aircraft but CFM56 powered tankers based on the E-3 design. 8 were sold to Saudi Arabia.[41]
E-3B
E-3As with improvements, 24 conversions.[41]
E-3C
Production aircraft with AN/APY-2 radar, additional electronic consoles and system improvements, ten built.[42]
JE-3C
One E-3A aircraft used by Boeing for trials later redesignated E-3C.[41]
E-3D
Production aircraft for the RAF to E-3C standard with CFM56 engines and British modifications designated Sentry AEW.1, 7 built.[41]
E-3F
Production aircraft for the French Air Force to E-3C standard with CFM56 engines and French modifications, 4 built.[41]
E-3G
USAF Block 40/45 modification.[42] Includes hardware and software upgrades to improve communications, computer processing power, threat tracking, and others, and automates some previously manual functions. initial operating capability (IOC) reached in July 2015.[43]

Operators

Map of the world with E-3-operating states highlighted in blue
 France
The French Air Force purchased 4 E-3F aircraft.
Assigned to the Escadron de Détection et de Commandement Aéroporté (ECDA, Air detection and command squadron) based at Avord Air Base.[44]
 NATO
Based in Geilenkirchen, Germany, 18 E-3 AWACS were purchased – 1 written off in Greece, 1 retired from service. For legal reasons these aircraft are officially registered as aircraft of Luxembourg, a NATO member without an air force.[26] Responsible for monitoring airspace for NATO operations around the world.
  • Aircrew Training Squadron[45]
  • Flying Squadron 1[46]
  • Flying Squadron 2[47]
  • Flying Squadron 3 – disbanded in 2015[48]
 Saudi Arabia
The Royal Saudi Air Force purchased five E-3A aircraft and eight KE-3A tanker aircraft in 1983.[49]
  • No. 18 Squadron
 United Kingdom
The Royal Air Force purchased 7 E-3Ds by October 1987 operating, six remain service; five are operational and one used for training, the other one has been withdrawn in March 2019.[50] The aircraft are designated Sentry AEW.1.[26]
8 Squadron[51]
23 Squadron (1996–2009)[52]
54 Squadron (Operational Conversion Unit)[51]
56 Squadron (Test and Evaluation)[51]
 United States
The United States Air Force currently has 32 E-3,
Tactical Air Command 1976–1992
Air Combat Command 1992–present
960th Airborne Air Control Squadron 2001–present (NAS Keflavik, Iceland 1979–1992)
963rd Airborne Air Control Squadron 1976–present
964th Airborne Air Control Squadron 1977–present
965th Airborne Air Control Squadron 1978–1979, 1984–present
966th Airborne Air Control Squadron 1976–present
968th Expeditionary Airborne Air Control Squadron 2002–2003, 2013–present[53]
Air Force Reserve Command
970th Airborne Air Control Squadron 1996–present
Pacific Air Forces
962d Airborne Air Control Squadron 1986–present
961st Airborne Air Control Squadron 1979–present

Incidents and accidents

Yukla 27 Memorial at Joint Base Elmendorf-Richardson.
LX-N90457, after having overrun the runway at Prevesa AB on 14 July 1996
Fire-damaged E-3 on Nellis AFB runway

The E-3 has been involved in three hull-loss accidents, and one radar antenna destroyed during RSIP development (see photo under Avionics).

  • On 22 September 1995, a U.S. Air Force E-3 Sentry (callsign Yukla 27, serial number 77-0354), crashed shortly after takeoff from Elmendorf AFB, Alaska. The plane lost power to both left side engines after these engines ingested several Canada geese during takeoff. The aircraft went down about 2 miles (3.2 km) northeast of the runway, killing all 24 crew members on board.[54][55]
  • On 14 July 1996, a NATO-operated E-3 Sentry (serial number LX-N90457) overran the runway and crashed into a sea wall at Préveza-Aktion Airport in Greece when the pilot attempted to abort takeoff after thinking the aircraft had ingested birds. There were no injuries, however, the fuselage broke, causing total loss of the aircraft. Upon investigation of the incident, there were no indications of bird ingestion.[56]
  • On 28 August 2009, a U.S. Air Force E-3C Sentry (serial number 83-0008) participating in a Red Flag exercise at Nellis AFB, Nevada experienced a nose gear collapse on landing, resulting in a fire and causing damage beyond repair. All 32 members of the crew evacuated safely.[57]

Specifications (USAF/NATO)

Data from Globalsecurity.org : E-3 Sentry (AWACS)[17]

General characteristics

  • Crew: Flight crew: 4 (aircraft commander, pilot, navigator, flight engineer)
Mission crew: 13–19
  • Length: 152 ft 11 in (46.61 m)
  • Wingspan: 145 ft 9 in (44.42 m)
  • Height: 41 ft 4 in (12.60 m)
  • Wing area: 3,050 sq ft (283 m2)
  • Empty weight: 185,000 lb (83,915 kg)
  • Gross weight: 344,000 lb (156,036 kg)
  • Max takeoff weight: 347,000 lb (157,397 kg)
  • Powerplant: 4 × Pratt and Whitney TF33-PW-100A turbofan, 21,500 lbf (96 kN) thrust each

Performance

  • Maximum speed: 461 kn (531 mph, 854 km/h)
  • Range: 4,000 nmi (4,600 mi, 7,400 km)
  • Service ceiling: 35,000 ft (11,000 m) (analog autopilot)

Avionics

  • AN/APS-133 colour weather radar
  • Westinghouse Corporation AN/APY-1 or AN/APY-2 passive electronically scanned array radar system

See also

Related development

Aircraft of comparable role, configuration, and era

Related lists

References

Notes

  1. ^ Quote:"...and the first flight of an E-3 with full mission avionics was from Seattle on 25 May 1976."[1]

Citations

  1. ^ Eden et al 2004, p. 94.
  2. ^ Wilson 1998, p. 72.
  3. ^ a b Eden et al. 2004, p. 92.
  4. ^ a b "AWACS to Bridge the Technological Gap". Air University. Archived from the original on 27 June 2004. Retrieved 14 February 2009.
  5. ^ a b c Davies 2005, p. 2.
  6. ^ Simonsen, Erik (March 2007). "Still keeping watch" (PDF). Boeing. Archived (PDF) from the original on 29 June 2011. Retrieved 21 August 2011.
  7. ^ Davies 2005, pp. 5–6.
  8. ^ a b "AWACS Surveillance Radar" (PDF). Northrop Grumman. Archived from the original (PDF) on 27 February 2009. Retrieved 10 February 2009.
  9. ^ Taylor et al. 1976, p. 246.
  10. ^ Piotrowski, General Pete. Basic Airman to General: The Secret War & Other Conflicts. p. 447. ISBN 978-1-4931-6186-7.
  11. ^ Gunston, Bill (1985). The Illustrated Encyclopedia of the World's Modern Military Aircraft. Leisure Books. ISBN 978-0-517-22477-9.
  12. ^ a b c d e f g h i j k l m n o p q Cite error: The named reference USAF1 was invoked but never defined (see the help page).
  13. ^ a b c d e "Airborne Warning and Control System (AWACS)". Boeing. Archived from the original on 18 May 2007. Retrieved 26 May 2007.
  14. ^ "Completes Mission System Flight Testing for US AWACS Block 40/45 Upgrade" (Press release). Boeing. 10 September 2008. Archived from the original on 29 June 2011. Retrieved 13 July 2011.
  15. ^ "EADS, Northrop Grumman, Partt and Whitney To Offer NATO AWACS Upgrade". Defense Daily International. 13 July 2001. Archived from the original on 6 November 2012. Retrieved 8 September 2010.
  16. ^ NATO summit Warsaw July 2016
  17. ^ a b "E-3 Sentry (AWACS): Specifications". globalsecurity.org. Archived from the original on 10 September 2011. Retrieved 18 August 2011.
  18. ^ "Boeing E-3 Airborne Warning and Control System (AWACS)" (PDF). Boeing. Archived from the original (PDF) on 18 March 2006. Retrieved 22 August 2011. {{cite web}}: Cite has empty unknown parameter: |1= (help)
  19. ^ "E-3 Sentry (AWACS)". globalsecurity.org. Archived from the original on 3 September 2009. Retrieved 9 November 2009.
  20. ^ Wilson 1998, p. 73.
  21. ^ "E-3 Sentry (AWACS)". Federation of American Scientists. 23 April 2000. Archived from the original on 19 June 2011. Retrieved 13 July 2011.
  22. ^ a b "E-3 Sentry (AWACS)". globalsecurity.org. Archived from the original on 12 May 2007. Retrieved 26 May 2007.
  23. ^ a b "AWACS For United Kingdom and France". Boeing. Archived from the original on 27 February 2007. Retrieved 26 May 2007.
  24. ^ https://www.nato.int/cps/en/natohq/declassified_147357.htm
  25. ^ "DRAGON program to improve aging E-3". af.mil. Archived from the original on 24 April 2018. Retrieved 14 April 2018.
  26. ^ a b c d e f g Wilson 1998, p 75.
  27. ^ a b "U.S. and NATO AWACS". Boeing. Archived from the original on 14 August 2011. Retrieved 21 August 2011.
  28. ^ "Military Safety". Flight International. 4–10 June 1997. p. 44. Archived from the original on 9 March 2012. Retrieved 23 August 2011.
  29. ^ https://shape.nato.int/resources/21/NATO%20Operations,%201949-Present.pdf
  30. ^ "AWACS For United Kingdom and France". Boeing. Archived from the original on 27 March 2011. Retrieved 26 September 2010.
  31. ^ "E-3 Specifications (707 Platform) and Worldwide Fleet". Boeing. Archived from the original on 27 March 2011. Retrieved 26 September 2010.
  32. ^ Hoyle, Craig. "RAF ISTAR watch: a Shadowy arrival, and saving Sentinel". Flightglobal. Archived from the original on 24 July 2013. Retrieved 27 September 2013.
  33. ^ Lake 2009, p. 44.
  34. ^ a b Veronico and Dunn 2004, p. 83.
  35. ^ ″The history of the TCA Squadron.″ Archived 28 May 2016 at the Wayback Machine NATO AWACS
  36. ^ "NATO starts patrolling Libyan air space". The Australian. 11 March 2011. Archived from the original on 2 February 2015. Retrieved 22 August 2011.
  37. ^ RAF Sentry AEW aircraft deploys in support of counter-IS mission Archived 2 February 2015 at the Wayback Machine – Flightglobal.com, 2 February 2015
  38. ^ "Archived copy". Archived from the original on 30 June 2015. Retrieved 7 July 2015.{{cite web}}: CS1 maint: archived copy as title (link)
  39. ^ "A NATO E-3A Arrives at Davis-Monthan AFB". dvidshub.net. Archived from the original on 14 April 2018. Retrieved 14 April 2018.
  40. ^ Boeing E-3G makes Middle East combat debut Archived 20 November 2015 at the Wayback Machine – Flightglobal.com, 19 November 2015
  41. ^ a b c d e f g h Pither 1998, pp. 40–42
  42. ^ a b "E-3 Sentry (AWACS) Variants". globalsecurity.org. Archived from the original on 10 September 2011. Retrieved 21 August 2011.
  43. ^ The wait is over…E-3 Block 40/45 deploys to combat theater Archived 20 November 2015 at the Wayback Machine – AF.mil, 18 November 2015
  44. ^ Wilson 1998, p 76.
  45. ^ https://web.archive.org/web/20161005091546/http://www.e3a.nato.int/eng/html/organizations/aircrew_training_sq.htm
  46. ^ https://web.archive.org/web/20160602204204/http://www.e3a.nato.int/eng/html/organizations/sq_1.htm
  47. ^ https://web.archive.org/web/20160612235226/http://www.e3a.nato.int/eng/html/organizations/sq_2.htm
  48. ^ https://web.archive.org/web/20161005093211/http://www.e3a.nato.int/eng/html/organizations/sq_3.htm
  49. ^ Wilson 1998, pp. 75–76.
  50. ^ "Wedgetail to be RAF's new early warning radar aircraft". Royal Air Force. 22 March 2019. Archived from the original on 22 March 2019. Retrieved 23 March 2019.
  51. ^ a b c "E-3D". Royal Air Force. Archived from the original on 23 March 2019. Retrieved 23 March 2019.
  52. ^ "23 Squadron". Royal Air Force. Archived from the original on 14 January 2011. Retrieved 23 March 2019.
  53. ^ "Factsheets : 968 Expeditionary Airborne Air Control Squadron (ACC)". www.afhra.af.mil. Archived from the original on 20 April 2016. Retrieved 4 April 2016.
  54. ^ "CVR transcript Boeing E-3 USAF Yukla 27–22 SEP 1995". Aviation Safety Network. 16 October 2004. Archived from the original on 12 October 2011. Retrieved 21 August 2011.
  55. ^ "Yukla 27". Airborne Early Warning Association. Archived from the original on 10 August 2011. Retrieved 22 August 2011.
  56. ^ Ranter, Harro. "ASN Aircraft accident Boeing E-3A Sentry (707-300B) LX-N90457 Préveza-Aktion Airport (PVK)". aviation-safety.net. Retrieved 24 September 2019.
  57. ^ "E-3 damaged while landing at Nellis AFB". Air Combat Command. Retrieved 24 September 2019.

Bibliography

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