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Boeing 737 AEW&C
The Boeing 737 AEW&C is a twin-engine airborne early warning and control aircraft. It is lighter than the 707-based Boeing E-3 Sentry, and mounts a fixed, active electronically scanned array radar antenna instead of a rotating one. It was designed for the Royal Australian Air Force (RAAF) under "Project Wedgetail" and designated E-7A Wedgetail. The 737 AEW&C has also been selected by the Turkish Air Force (under "Project Peace Eagle", Turkish: ''Barış Kartalı'') and the Republic of Korea Air Force ("Project Peace Eye", Korean: "피스 아이"), and has been proposed to Italy and the United Arab Emirates.
==Design and development==
In the 1990s, Australia began forming a need for an airborne early warning and control (AEW&C) aircraft. In 1996, Australia issued a request for proposal (RFP) for the aircraft for the RAAF under ''Project Wedgetail''.〔("AIR 5077 - Project Wedgetail" ). Defence Materiel Organisation〕 In 2000, Australia awarded Boeing Integrated Defense Systems a contract to supply four AEW&C aircraft with options for three additional aircraft.
The 737 AEW&C is based on Boeing Business Jet 1; a 737-700IGW airframe variant of the Boeing 737 Next Generation, roughly similar to the 737-700ER. The aircraft uses the Northrop Grumman Electronic Systems Multi-role Electronically Scanned Array (MESA) radar. The L-band (1 to 2 GHz) electronically scanned AEW and surveillance radar is located on a dorsal fin on top of the fuselage, dubbed the "top hat", and is designed for minimal aerodynamic effect. The radar is capable of simultaneous air and sea search, fighter control and area search, with a maximum range of over 600 km (look-up mode). When operating in look-down mode against fighter-sized target, the maximum range is in excess of 370 km. When used against maritime targets, the maximum range is over 240 km for frigate-sized targets. MESA is capable of simultaneously tracking 180 targets and conducting 24 intercepts. In addition, the radar antenna array is also doubled as an ELINT array, with a maximum range of over 850 km at 9,000 meter altitude.〔(Jane's Radar and Electronic Warfare Systems,2011-2012 edition )〕 The 10.8 m long by 3.4 m high antenna assembly incorporates 7.3 m long by 2.7 m high Side-Emitting Electronic Manifold array, with the top hat supporting array providing 120° coverage on port and starboard side, while the top hat array itself provides 60° fore and aft, thus providing a complete 360° coverage. The radar's beam can be set for a 2° to 8° width, while scan duration can be set from 3 s to 40 s. Radar signal processing equipment and central computer are installed directly below the antenna array.〔(Jane's Electronic Mission Aircraft, 2011 Edition )〕
Other modifications include ventral fins to counterbalance the radar and countermeasures mounted on the nose, wingtips and tail. In-flight refueling is via a receptacle on top of the forward fuselage. The cabin features eight operator consoles with sufficient space for four more; the Australian fleet will operate ten consoles with space for two more (four on port side and six on the starboard side).〔(Jane's all the World's Aircraft, 2011-2012 Edition )〕 Northrop Grumman's MESA radar also formed the basis for the same company's Multi-Platform Radar Technology Insertion Program (MP-RTIP) which was developed for the United States Air Force's E-10 MC2A aircraft.
抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』
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