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A Magnetic Anomaly Detector(MAD) 'stinger' was added to the tailcone, a search radar was added in the nose, and a fin-tip radome ('football') was fitted to accommodate ESM equipment. A new ventral weapons pannier was added beneath the cabin, giving a distinctive 'double-bubble' cross-section, these changes necessitating an increase in fin area. In the front of this cabin there is the search radar. The windshield of the cockpit is enlarged. A searchlight is added in the right wing. The first prototype was powered by the production Nimrod's intended Rolls Royce Spey engines and made its maiden flight on 23rd May 1967, serving as an aerodynamic test-bed and for airframe/engine integration. The second retained Avons and flew on 31 July, serving as the avionics development aircraft.
The MR.MK1 uses 4 RB.168-200 "Spey" turbofan engines, each power 5506kg. The whole fuel capability is up to 38940kg. With the 6 disassembly fueltanks in the cabin, it can be added to 45785kg. There 12 crew onboard, including two pilots and one engineer in the cockpit, navigator, tactical navigator, radio operator, radar operator, two sonar operators, ECM and MAD operator and two surveillance and cargo operator. The sonar system is in the afterbody, includes types of sonar buoys, all loaded on the launchers. The weapons for a single MP.MK1 includes nine torpedos and bombs and the weapon cabin gets a warming system to keep the weapon in standby condiction. From 1975 the 35 remaining MR.MK1s were upgraded to MR.MK2 configuration, the first MR.MK2 being redelivered to the RAF in August 1979. The MR.MK2 had a completely new avionics and equipment suite, in which all major sensors and equipment items were changed. The aircraft received a new Marconi GEC central tactical system, based on a new FM1600D computer and three separete 920ATC processors for navigation systems, radar and acoustic sensors. The old ASV-21D radar is replaced by a Thorn EMI Searchwater, which now has a colour display. The radar system can distinguish the ships, the air tube and the periscope at its largest operation range. The acoustics system is based on AQS901 sonar system, compatible with BARRA, SSQ-41 and SSQ-53, TANDEM, and Ultra active and passive sonobuoys. Communications equipment is similarly upgraded, including two AS470 radio and encrypt system. The addition of inflight-refuelling probes (initially to 16 aircraft for participation in Operation Corporate) changed the aircraft designation of MR.MK2P and necessitated the addition of tiny swept finlets on the tailplanes. The Falklands War also resulted in the underwing hardpoints being used by front-line Nimrods for the first time, giving the ability to carry AIM-9 Sidewinders for self-defence, or anti-ship Harpoon missiles, Stingray torpedoes, bombs or depth charges. The planned wingtip Loral ARI.18240/1 ESM pods were added later, these requiring larger rectangular finlets. All aircraft now have both refuelling probes and ESM pods. For operation from Seeb in Oman, during Operation Desert Storm, a number of Aircraft were drawn from Nos 120 (lead), 42 and 206 Sqns to form the Nimrod MR Detachment. Several were modified to what was (unofficially) referred to as Nimrod MR.Mk 2P(GM)(Gulf Mod) through the addition of an underwing FLIR turret on the starboard wing, BOZ pods and a TRD (Towed Radar Decoy).
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BAE now is selected as the prime contractor in July 1996 to supply a complete package of 21 mission-equipped Nimrod 2000 aircraft, together with a training system and initial logistic support. It is planned that MR.MK2 fuselage and empennage structure would be re-lifed and reassembled, with redesigned wings and BR710 turbofan engines. The flight deck is imporved, which will accommodate a reduced cockpit crew complement to eight, facilitated by automated flight systems using modified Airbus A340 technology. The mission system is entirely new. The cabin interior is totally refitted to suit the new mission systems layout. An underwing hardpoint on each side of the aircraft can carry the Boeing AGM-84 Harpoon anti-ship missile or the AIM-9 Sidewinder air-to-air missile from Lockheed Martin and Raytheon.
In early 1998 the aircraft was renamed from Nimrod 2000 to Nimrod Maritime Reconnaissance and Attack Mk4 - Nimrod MRA4. Nimrod MRA4 is equipped with a Navigation and Flight Management System (NAV/FMS) from Smiths Industries. It consists of a navigation computer and flight management computer which are interfaced to the aircraft's MIL-STD-1553B data bus. The sensors include a laser inertial navigation system, two LN-100G Global Positioning Systems from Litton, radio navigation, a microwave landing system and a TCAS 2 Traffic Alert and Collision Avoidance System. MRA4 has a Searchwater 2000MR multi-mode search radar from Racal and an electro-optical surveillance and detection system, EOSDS, supplied by Northrop Grumman. It is also equipped with a radar warning receiver, an Elta electronic support measures system and magnetic anomaly detector (MAD) system. For reasons, the project was delayed and dued to serve in 2001. In 2002, the Defense Department of UK cut down the requirement of MRA4 from 21 to 18. Because the Department realized that there are no more increased threatening from the sea these years, and the decreased 3 aircrafts would not effect the battle effectiveness. On 26 August 2004, PA1, the first of three Nimrod MRA4 development aircraft took off from BAE SYSTEMS Woodford site on the historic first flight of Nimrod MRA4, landing some 2 hours later at BAE SYSTEMS Warton following a successful maiden test flight. See the accompanying photographs.Min(DP), who was at Warton at the time, made the following statement after the aircraft had landed: "I was delighted to have been present for the first flight of Nimrod MRA4. It represents a significant milestone in a programme which has presented a number of challenges for BAE Systems and its supply chain. I now look forward to a successful series of flight trials towards proving a mature production design which meets MOD¡¯s requirements and to the agreement of satisfactory prices for production." The successful completion of the first flight is a significant milestone in the Nimrod MRA4 programme. This is a major achievement for British industry and for the BAE SYSTEMS workforce and for its Supply Chain. It is the culmination of many years of effort. It is, however, just one step on the way to the completion of the design and development phase of the Nimrod MRA4 programme. Work must continue on the test and evaluation programme. We look forward to the first flight of the second aircraft (PA2) later this year and the third aircraft (PA3) next summer. These aircraft will be used for mission system proving and weapon handling trials. Nimrod MRA4 aircraft will offer greater capability, availability and endurance when compared to the Nimrod MR2 fleet, and our maritime surveillance requirements could be met with a fleet of around 12 Nimrod MRA4 aircraft. Any commitment to full production will be dependent on acceptable design maturity and the agreement of an acceptable price.
MRA4 cockpit
MRA4 BR710
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Specification Length 38.63m Maximum Normal Take-off Weight 80514kg
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