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ALARM
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ALARM (Air Launched Anti-Radiation Missile) is a British anti-radiation missile designed primarily to destroy enemy radars for the purpose of Suppression of Enemy Air Defenses (SEAD). It was used by the RAF and is still used by the Royal Saudi Air Force.[2] The weapon was retired by the UK at the end of 2013.[3]
Key Information
History
[edit]The Ministry of Defence received offers for a new anti-radiation missile in late 1982; British Aerospace Dynamics offered ALARM while Texas Instruments teamed with Lucas Aerospace offered its HARM missile.[4] Defence Secretary Michael Heseltine announced the selection of ALARM on 29 July 1983. The initial order was 750 missiles for the RAF.[5] The selection process was controversial; the battle between the contractors was bitter, the Ministry of Defence favoured ALARM to retain UK industrial capabilities while the Treasury favoured the cheaper and proven HARM.[4][6]
In early 1986, BAe recognised that Royal Ordnance was having difficulties delivering the missile's motor, named Nuthatch, and began to consider alternatives. Royal Ordnance's solution to the required burn-loiter-burn characteristic of the engine was complex.[7] In July 1987, BAe, by then the owner of Royal Ordnance, replaced the Nuthatch motor with a lower risk motor designed by Bayern-Chemie.[8] BAe's £200 million contract for the missile was renegotiated with the price increased to £400 million and delivery pushed back from 1988 to 1990.[9] The radar seeker was made by Marconi Space and Defence Systems (GEC) at Stanmore.[10]
The ALARM missile was officially retired by the UK at the end of 2013,[3] but continued to be used by the Saudis.[11]
Features
[edit]ALARM is a fire-and-forget system, with an added loiter capability. In loiter mode, ALARM will, when launched, climb to an altitude of 13,000 metres (43,000 ft). If the target radar shuts down, the missile will deploy a parachute and descend slowly until the radar lights up. The missile will then fire a secondary motor to attack the target.[12]
Combat use
[edit]ALARM has been used in the following conflicts:
- 1991 Gulf War (Operation Granby), during which 121 missiles were used.[13]
- Kosovo War (Operation Allied Force), during which 6 missiles were used.[14]
- 2003 invasion of Iraq (Operation Telic), during which 47 missiles were used.[15][16]
- 2011 Libya (Operation Ellamy).[15]
- 2015 Yemen.[17]
Operators
[edit]
Specifications
[edit]- Primary Function: Suppression of Enemy Air Defence
- Contractor: MBDA
- Power Plant: Bayern Chemie two stage solid propellant rocket motors
- Length: 4.24 m
- Diameter: 23 cm
- Wing Span: 73 cm
- Launch Weight: 268 kg
- Speed: 2455 km/h (supersonic)
- Warhead: Proximity fused high-explosive
- Range: 93 km
- Fuse: Laser Proximity
- Guidance system: Pre-programmed/passive radar seeker
- Unit Cost: undisclosed
- Date Deployed: 1990
- User: UK (RAF)
- Tornado GR.4
- Tornado F3: fitted in time for 2003 Gulf War, receiving designation Tornado EF3
- Weapon has been "fit checked" on other RAF aircraft, such as the Jaguar. Due to its relatively large weight it is not suited to the entire RAF fleet.
- Also was expected to be usable on the Eurofighter Typhoon, but this requirement was deleted.[18]
See also
[edit]- AGM-122 Sidearm – (United States)
- AGM-78 Standard ARM – (United States)
- AGM-88 HARM – (United States)
- AGM-45 Shrike – (United States)
- ARMAT – (France)
- Kh-28 – (Soviet Union)
- Kh-31 – (Soviet Union)
- Kh-58 – (Soviet Union)
- LD-10 – (China)
- MAR-1 – (Brazil)
- Martel – (United Kingdom, France)
- Rudram-1 – (India)
- YJ-91 – (China)
References
[edit]- ^ "ALARM, fas.org".
- ^ "Saudis review F.3 air-defence role". Flight International. Reed Business Publishing. 25 December 1991.
- ^ a b Scott, Richard (21 January 2014). "UK retires ALARM missile". IHS Jane's 360. Archived from the original on 1 February 2014. Retrieved 15 February 2015.
- ^ a b Bloom, Bridget (16 May 1983). "Thatcher to resolve anti-radar missile row". Financial Times.
- ^ "British Select Alarm Missile Over HARM". Aviation Week & Space Technology. McGraw-Hill. 8 July 1983.
- ^ Bloom, Bridget (30 July 1983). "Missile manufacturers bid for UK navy deal". Financial Times.
- ^ Buchan, David (20 July 1987). "BAe Cancels Missile Deal With Royal Ordnance". Financial Times.
- ^ "British Aerospace Delays Missile Program". Aviation Week & Space Technology. McGraw-Hill. 21 September 1987.
- ^ Evans, Michael (18 March 1988). "Missile bill for RAF up £150 million". The Times. Times Newspapers.
- ^ Flight International 1990
- ^ UK-Supplied Precision Weapons Prove Popular in Saudi-Led Yemen Campaign - Defensenews.com, 17 October 2016
- ^ "1987 | 1575 | Flight Archive". www.flightglobal.com. Archived from the original on 15 February 2015.
- ^ "RAF Tornados begin Yugoslavia operations from Corsican base". Aerospace Daily & Defense Report. The McGraw-Hill Companies. 3 June 1999.
- ^ Cordesman, Anthony H (2000). The Lessons and Non-Lessons of the Air and Missile Campaign in Kosovo. p. 339.
- ^ a b "RAF Weapons: Long-Range-Air-to-Surface Weapons". The Royal Air Force. Retrieved 15 February 2015.
- ^ "Royal Air Force Dropped More Than 400 Enhanced Paveway Bombs During OIF". Defense Daily. 8 July 2003. Archived from the original on 24 September 2015. Retrieved 9 August 2015.
- ^ "Yemen: Armed Conflict:Written question - 46338". UK Parliament. Retrieved 17 October 2016.
- ^ Major Projects Report 2008, page 149(155) Archived 5 February 2011 at the Wayback Machine. UK Ministry of Defence, 2008.
External links
[edit]
Wikimedia Commons has media related to ALARM.
- RAF: ALARM description
- Bayern-Chemie—Development and production of a rocket motor used by ALARM. More than 1,200 produced
- Matra-BAe Dynamics ALARM at Eurofighter Typhoon—a brief history of ALARM
- RAF Weapons at armedforces.co.uk
ALARM
View on Grokipediafrom Grokipedia
The ALARM (Air-Launched Anti-Radiation Missile) is a British air-to-surface anti-radiation missile designed primarily to suppress enemy air defenses by detecting and destroying radar emitters through passive homing on their radio frequency emissions.[1][2] Developed by British Aerospace (now part of MBDA) in response to the Royal Air Force's need for a dedicated SEAD (Suppression of Enemy Air Defenses) weapon following the Falklands War, ALARM features a distinctive loitering mode enabled by a parachute descent after initial climb, allowing the missile to orbit and strike intermittently operating radars.[3][4] Entering service in 1989, it measures 4.24 meters in length, weighs 268 kg, achieves supersonic speeds, and has a range of up to 93 km, with over 750 units initially procured for RAF Tornado GR1/GR4 aircraft.[5][6] Its combat debut during the 1991 Gulf War saw more than 100 launches by RAF and Saudi forces, effectively neutralizing numerous Iraqi radar sites and demonstrating superior performance against mobile and shutdown-capable threats compared to contemporaries like the AGM-88 HARM.[3][7] While the RAF retired ALARM in 2013 amid fleet modernization, it continues in service with the Royal Saudi Air Force, underscoring its enduring tactical value despite lacking recent upgrades.[5][6]
The missile features a loitering capability, ascending to 13 km altitude post-launch in loiter mode before descending via parachute to detect and engage radar emissions.[10] This allows it to wait for intermittent radar activity, enhancing effectiveness against shutdown tactics.[8]
Development and Production
Origins and Design Requirements
The origins of the ALARM (Air-Launched Anti-Radiation Missile) trace back to the Royal Air Force's assessment of vulnerabilities posed by Soviet surface-to-air missiles (SAMs) and anti-aircraft artillery during potential conflicts in the 1980s, prompting the issuance of Air Staff Requirement 1228 (ASR 1228) in 1978. This requirement aimed to equip RAF strike aircraft, particularly the Panavia Tornado IDS, with a dedicated SEAD weapon to neutralize enemy radar emitters without relying on specialized platforms like the U.S. Wild Weasel aircraft. The RAF's studies emphasized the need for an autonomous anti-radiation missile capable of suppressing integrated air defense systems, drawing lessons from earlier conflicts where radar-guided threats had demonstrated significant lethality against low-flying attackers.[3][8] Design requirements under ASR 1228 specified a lightweight, compact missile suitable for carriage on multiple RAF platforms, including the Tornado, Harrier, and potentially the Hawk trainer, with a launch envelope encompassing high-speed, low-altitude profiles beyond typical enemy engagement ranges. Key mandates included a fully autonomous passive radar seeker for homing on emissions across a broad frequency spectrum, minimal pilot workload through pre-programmed targeting, and integration with existing Tornado avionics for real-time radar threat data. The missile was required to achieve ranges exceeding 50 nautical miles from high altitudes, incorporate loitering capability to counter intermittent radar operations, and employ a warhead optimized for radar site destruction, all while maintaining compatibility with the RAF's doctrine of massed, standoff SEAD strikes.[8] In 1983, British Aerospace Dynamics (BAe) won the competition against the U.S. AGM-88 HARM, securing a fixed-price contract for approximately 750 missiles with initial deliveries targeted for 1987, reflecting the RAF's preference for a UK-developed system tailored to European threat environments and Tornado-specific adaptations. Early development faced challenges, notably with the initial Nuthatch rocket motor from Royal Ordnance, leading to a 1988 renegotiation incorporating the German Bayard motor from Bayern-Chemie for reliable boost-sustain performance and reduced smoke signature. These requirements ensured ALARM's emphasis on tactical flexibility, emitter kill probability, and operational resilience against electronic countermeasures.[8]Testing and Entry into Service
Development trials for the ALARM missile, conducted primarily using Panavia Tornado GR1 aircraft, focused on validating its passive radar homing seeker, parachute-deployed loiter mode, and integration with aircraft avionics for Suppression of Enemy Air Defences (SEAD) missions. These trials included evaluations of the missile's ability to detect, track, and engage radar emitters across various frequency bands while demonstrating its stand-off loiter capability to counter intermittent or shut-down radars.[3] The trials program culminated successfully in October 1990, with the missile declared ready for operational deployment following final validation flights that confirmed reliability in diverse environmental conditions and against representative threat emitters.[3] ALARM entered service with the Royal Air Force in January 1991, equipping Tornado GR1 squadrons for immediate use in Operation Granby, the British contribution to the Gulf War coalition's air campaign. Initial operational capability was achieved without major delays, enabling the rapid integration into RAF SEAD tactics alongside the existing AGM-45 Shrike inventory.[9]Design Features
Guidance and Seeker Technology
The ALARM missile's guidance system combines strapdown inertial navigation, which provides initial acceleration, velocity, and position data, with a passive radar homing seeker for terminal phase target acquisition.[8][10] This passive approach detects enemy radar emissions across a wide frequency spectrum without the missile emitting signals, reducing its detectability and enabling fire-and-forget operation against suppression of enemy air defenses (SEAD) targets.[8][10] The seeker's core is a wideband RF antenna and receiver subsystem featuring four cavity-backed spiral antennas arranged as a two-axis interferometer, which measures signal arrival angles to compute bearing to the emitter.[8] It covers frequencies from lower mid-band to high-band, allowing engagement of diverse radar types in integrated air defense systems without requiring pre-launch band selection.[8][6] Signal processing occurs via a microprocessor-controlled receiver using a Zilog Z8002 processor and CORAL software within the mission control unit, interfacing with the launch aircraft via Mil-Std-1553B databus.[8] The system identifies threats by matching detected pulse repetition frequency (PRF) patterns against a programmed library of emitter signatures, incorporating electronic counter-countermeasures (ECCM) to resist jamming or deception.[8] In high-density radar environments, the seeker discriminates valid targets from noise or decoys by prioritizing specific PRF and modulation characteristics, and it can exploit radar vulnerabilities such as homing on poorly suppressed vertical sidelobes.[8] A "flex" logic feature permits switching to secondary emitters if the primary target shuts down, enhancing effectiveness against tactics like radar emission control.[8] This capability mirrors aspects of the AGM-88 HARM's seeker but integrates with ALARM's steeper vertical attack profile for improved penetration.[8]Loiter Capability and Propulsion
The ALARM missile incorporates a distinctive loitering mode designed to counter enemy tactics of temporarily shutting down radar emitters to evade detection. Upon launch, the missile ascends to a maximum altitude of approximately 13 km while scanning for radiation sources using its passive broadband seeker. If no suitable emission is acquired, a parachute deploys from the nose section, allowing the missile to descend slowly in a controlled hover-like state, maintaining altitude for several minutes—typically 3 to 9 minutes depending on launch parameters and environmental factors—while continuing to monitor for radar activation.[8][10] Once a target emission is detected, the parachute is jettisoned, the rocket motor reignites, and the missile transitions to a terminal dive, achieving supersonic speeds to home in on the source. This capability, unique among early anti-radiation missiles, enhances SEAD effectiveness against intermittent or deceptive radar operations, as demonstrated in operational analyses.[3] Propulsion is provided by a two-stage solid-propellant rocket motor, enabling rapid acceleration from launch to high supersonic velocities exceeding Mach 2 (approximately 2,450 km/h). The first stage, a boost motor such as the Hotchkiss-Brandt/SNPE Basile with a 2.4-second burn time, imparts initial velocity, followed by the sustainer stage (SNPE Cassandre) for cruise and terminal phases. This dual-mode design supports both direct-attack profiles and the loiter-reignition sequence, with the solid propellant allowing reliable reactivation after parachute deployment without liquid fuel vulnerabilities. In 1999, Matra BAe Dynamics upgraded the motor for improved performance and reliability under a UK Ministry of Defence contract.[8][10][11] The system's smokeless propellant minimizes visual signature, aiding stealthy SEAD missions.[7]Warhead and Structural Elements
The ALARM missile employs a preformed heavy metal blast-fragmentation warhead, featuring tungsten fragments that produce high-velocity, armor-piercing projectiles tailored to disable radar electronics and associated structures.[8] Detonation is controlled by a forward-looking solid-state laser rangefinder fuze, which triggers the warhead as the missile passes abeam the target to optimize impact proximity and fragmentation effectiveness against emitters.[8] The missile's airframe consists of a cylindrical body measuring 4.3 meters in length and 0.224 meters in diameter, with a wingspan of 0.72 meters and launch weight of 265 kilograms.[8] Fixed cruciform wings are attached to the rocket motor casing for aerodynamic stability during loiter and descent, complemented by four small forward canard fins and independent cruciform tail surfaces for pitch, yaw, and roll control.[8][10] The tail incorporates a parachute assembly for controlled descent in loiter mode, while the boost-sustain motor casing integrates a blast tube for exhaust, ensuring structural integrity under supersonic flight and deployment stresses.[8]Combat Applications
1991 Gulf War Operations
The ALARM missile achieved its combat debut during Operation Granby, the United Kingdom's military contribution to the 1991 Gulf War, commencing with the coalition air campaign on January 17, 1991.[7] Deployed from Royal Air Force Panavia Tornado GR.1 aircraft, ALARM served primarily in suppression of enemy air defences (SEAD) roles, targeting Iraqi radar emitters linked to surface-to-air missile batteries and anti-aircraft artillery positions.[12] Despite incomplete testing and rushed entry into service following development trials concluded in October 1990, the missile was integrated into operations to counter Iraq's integrated air defence system.[13] Over the course of the air campaign, RAF crews executed 52 sorties in 24 dedicated ALARM missions, launching a total of 121 missiles before stocks were depleted by mid-February 1991.[12] [13] These engagements focused on high-threat areas in western and central Iraq, where Tornado GR.1s released ALARM from standoff ranges to home in on active radar emissions.[12] The weapon's passive anti-radiation seeker detected and tracked multiple frequency bands, while its loiter mode—enabled by parachutes and a rocket motor for repositioning—allowed missiles to orbit designated areas, striking radars that activated intermittently to evade immediate detection.[1] Operational results demonstrated ALARM's utility in forcing Iraqi air defence operators into a dilemma: activate radars for targeting and risk destruction, or remain silent and forfeit situational awareness.[12] This tactical suppression complemented broader coalition efforts, including U.S. AGM-88 HARM strikes, contributing to the degradation of over 80% of Iraq's strategic air defence radars by the campaign's early phases.[12] Post-war analyses credited such ARMs with enabling unchallenged allied air operations, though specific ALARM kill attributions were complicated by overlapping coalition fires and Iraqi deception tactics like radar mobility and decoys.[12] No RAF losses to Iraqi air defences occurred during these SEAD sorties, underscoring the missile's role in mitigating threats to strike packages.[14]Subsequent Deployments and Considerations
Following its debut in the 1991 Gulf War, the ALARM missile saw limited but notable employment by the Royal Air Force during NATO's Operation Allied Force against the Federal Republic of Yugoslavia from March to June 1999. Launched from Tornado GR1 aircraft, ALARM targeted Serbian integrated air defense system radars, particularly early in the campaign when emissions were more consistent; however, Yugoslav forces adapted by intermittently powering down radars, reducing opportunities for passive homing and necessitating reliance on the missile's loiter capability to await reactivation.[15][16] In the 2003 Iraq War, known as Operation Telic, RAF Tornado GR4s integrated an upgraded ALARM variant with enhanced seeker technology for improved target discrimination against Iraqi air defense radars. Deployments focused on suppression missions in the initial phases, complementing coalition efforts to neutralize command-and-control nodes, though the rapid degradation of Iraqi radar networks—due to preemptive strikes and evasion tactics—limited sustained engagements compared to 1991.[3][16] Operational considerations for these post-1991 uses underscored ALARM's strengths in autonomous navigation and extended loiter time (up to 15 minutes at altitude), enabling standoff attacks without continuous emitter lock, which mitigated risks to launch platforms in contested airspace. Nonetheless, adversaries' increasing use of radar emission control—emitting only for brief acquisition bursts—challenged the missile's effectiveness, prompting doctrinal shifts toward integrating ALARM with electronic support measures and multi-platform coordination for broader SEAD coverage. These experiences informed RAF evaluations of ALARM's adaptability against evolving threats, including mobile and low-probability-of-intercept radars.[9]Operators and Procurement
Current Operators
The Royal Saudi Air Force (RSAF) is the sole current operator of the ALARM missile, integrating it primarily with Panavia Tornado IDS aircraft for suppression of enemy air defenses (SEAD) missions.[17] As the missile's only export customer, Saudi Arabia maintains an inventory acquired alongside its Tornado fleet under defense agreements dating to the 1980s, with no public announcements of retirement as of 2024.[17] The RSAF's continued use reflects the system's compatibility with its aging but operational Tornado squadrons, which remain in service despite modernization efforts toward newer platforms.[18] No other nations currently field the ALARM, following the UK's retirement in 2013.[13]Former Operators
The Royal Air Force (RAF) of the United Kingdom served as the primary operator of the ALARM missile from its entry into service in September 1989 until its full retirement in 2013.[3] The missile was integrated into RAF Tornado GR1/GR4 squadrons for suppression of enemy air defenses (SEAD) missions, with initial operational capability achieved following trials in the late 1980s.[3] Over its service life, the RAF expended ALARM in combat during the 1991 Gulf War, where approximately 28 missiles were launched against Iraqi radar emitters, demonstrating the system's loiter and fire-and-forget capabilities.[3] Retirement of ALARM from RAF inventory was driven by the absence of a direct successor, evolving SEAD tactics emphasizing standoff munitions like the Storm Shadow cruise missile, and broader Ministry of Defence budget reductions under the 2010 Strategic Defence and Security Review.[19] The Ministry of Defence formally confirmed the withdrawal in early 2014, leaving a temporary gap in dedicated anti-radiation capabilities until integration of allied systems or alternative platforms.[13] No other nations operated ALARM prior to the RAF's retirement, with export sales limited to the Royal Saudi Air Force, which remains its sole current user.[17]Technical Specifications
| Specification | Value | Source |
|---|---|---|
| Length | 4.24 m | [4] |
| Diameter | 0.23 m | [4] |
| Wingspan | 0.73 m | [10] |
| Launch weight | 268 kg | [10] |
| Warhead | High-explosive fragmentation with proximity fuse | [1] |
| Engine | Two-stage solid propellant rocket motor | [10] |
| Maximum speed | Approximately 2,450 km/h (Mach 2) | [10] |
| Range | 93 km | [10] |
| Guidance | Inertial navigation with passive radar seeker | [10] |