This is what was posted on this site in April 2017: “MBDA is planning integration of Meteor on the Lockheed Martin F-35 Lightning II Block 4. Raytheon's staged approach to meeting the full SR(A)1239 requirement offered an interim weapon with a capability between the AIM-120B AMRAAM and the FMRAAM. The weapon’s electronics and propulsion control unit (ECPU) adjusts the cruise speed depending on launch conditions and the target’s altitude by controlling the ramjet’s intake ducts. This took place against a backdrop of government and industrial contacts between the UK, France, and Germany aimed at establishing a common requirement and an industrial consortium. The trade-off between winged and wingless configurations was very closely balanced but the wings offered increased roll damping which was believed to be useful given the asymmetric intake configuration so the German A3M configuration was adopted for the European proposal, called Meteor. In April 2004 MBDA carried out fit checks on a Gripen at Saab's Linköping facility. Meteor was selected in competition to meet the UK's Staff Requirement (Air) 1239 (SR(A)1239), for a Future Medium Range Air-to-Air Missile (FMRAAM) to replace the RAF's BAe Dynamics Skyflash missiles. View all posts by Ed Jackson →. This feature of the EPCU helps the missile to manage its fuel system. The missile debris was recovered and the air intakes were found to be still closed.[86]. Over the eight months following contract signature, MBDA had determined the definitive external shape of Meteor. Meteor’s stunning performance is achieved through its unique ramjet propulsion system – solid fuel, variable flow, ducted rocket. Surely this could be a replacement for Astor and a mixed system would not only benefit the army (I know the army doesn’t use Astor, but only has short range air defences) but also the navy, if both could use the mark41 launcher on Royal Navy ships! For the first time, Europe will equip its fighter aircraft with a European air-to-air missile, creating interoperability and independence to export". The maiden test firings of Meteor from Gripen aircraft were conducted in 2006 at the Vidsel range in Sweden.

[46] These delays led to high-level diplomatic contacts over the summer with both the UK and Italian Defence ministers writing to their German counterpart stressing the importance of the Meteor programme. In addition to it’s active radar guidance seeker, which is shared with the MICA and ASTER series of missiles, the Meteor possesses two-way data link capabilities that allow it to continue communication with the targeting systems on the airframe it was fired from which itself may be receiving linked targeting information from other sources. The guidance section also has its own IMS or inertial measurement system, enabling the missile to ‘dead reckon’ it’s location in the battle space relative to where it was launched from in it’s terminal phase. The Meteor programme sees the UK, France, Germany, Italy, Spain and Sweden working together to provide access to technology and expertise across those nations. The Meteor missile is powered by a solid fuel variable flow ducted rocket (ramjet) supplied by Bayern-Chemie. Following several rounds of bid clarification it was concluded in early 1997 that the risks were too high to proceed directly to development. In July 1998 a formal statement of intent was signed between the governments of the UK, Germany, Italy, Sweden, and Spain which, subject to the UK's selection of Meteor, agreed to work towards joint procurement of the same missile. By February 1996 the U.S. team was in place whereas the European effort remained fragmented. TDR propulsion provides a long range, a high average speed, a wide operational envelope from sea level to high altitude, a flexible mission envelope via active variable thrust control, relatively simple design, and logistics similar to those of conventional solid-fuel rocket motors.[66]. The gas generator is ignited by the hot gases from the booster combustion which flow through the open control valve. The initial results suggested that the attenuation was much less than expected. IIR wouldn’t be much use at range either, MMW would be used. [66] The launch conditions were the same as the first two firings but the missile flew a different flight profile. It also notifies target acquisition by the seeker. So the modification will be used on all Meteors regardless of aircraft fit. An incremental approach would allow any technological advances to be incorporated into future upgrades. [96][97] The Meteor has already been checked for fit in the internal weapons bays of the JSF. It’s just the fins. Just as guideline. To ensure total target destruction, the missile is equipped with both impact and proximity fuses and a fragmentation warhead that detonates on impact or at the optimum point of intercept to maximise lethality.”. By the summer of 2005 two inert missiles had been delivered to Modane to recommission the facility following major modifications intended to prepare it for the free-jet trials.

In autumn 1999 Raytheon offered yet another twist to its staged approach with the ERAAM+. The programme will be managed by the UK MoD through the IPT on behalf of the partner nations. The gas generator contains an oxygen deficient composite solid propellant which produces a hot, fuel-rich gas which auto-ignites in the air which has been decelerated and compressed by the intakes. On 5 September 2006 the third and final ALD firing was successfully conducted. [37] The decision was so politically delicate that some believed that the EAC would leave it to the Prime Minister when he chaired the defence and overseas policy committee.

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