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BAir defence
series of surface-to-air anti-ballistic missile and anti-aircraft defense systems
At a glance
Measured figures
Length
Single source12 ft (3.7 m)[source]
Sky Bow III only; retired Sky Bow I values not inherited · Length
Single sourceConfiguration
| Specification | RIM-7 Sea Sparrow | Sky Bow |
|---|---|---|
| Type | Surface-to-air missile[source] | series of surface-to-air anti-ballistic missile and anti-aircraft defense systems[source] |
| Place of origin | United States[source] | — |
| In service | 1976–present[source] | The TK-2, TK-3 and TK-4 are in service with the Military of the Republic of China[source] |
| Manufacturer | Raytheon and General Dynamics[source] | National Chung-Shan Institute of Science and Technology (NCSIST) |
Sky Bow II only; retired Sky Bow I values not inherited · Length
Single source5.673 m[source]Sky Bow II only; retired Sky Bow I values not inherited
5.498 m[source]Sky Bow III only; retired Sky Bow I values not inherited
Diameter
Single source8 in (20 cm)[source]
Sky Bow III only; retired Sky Bow I values not inherited · Diameter
Single sourceSky Bow II only; retired Sky Bow I values not inherited · Diameter
Single source0.42 m[source]Sky Bow II only; retired Sky Bow I values not inherited
0.4 m[source]Sky Bow III only; retired Sky Bow I values not inherited
Mass
Single source510 lb (230 kg)[source]
Sky Bow III only; retired Sky Bow I values not inherited · Mass
Single sourceSky Bow II only; retired Sky Bow I values not inherited · Mass
Single source1,135 kg[source]Sky Bow II only; retired Sky Bow I values not inherited
870 kg[source]Sky Bow III only; retired Sky Bow I values not inherited
Operational; Operational range
Single source10 nmi (19 km)[source]
Sky Bow III only; retired Sky Bow I values not inherited · Range
Single sourceSky Bow II only; retired Sky Bow I values not inherited · Range
Single source150 km[source]Sky Bow II only; retired Sky Bow I values not inherited
200 km[source]Sky Bow III only; retired Sky Bow I values not inherited
Sky Bow II only; retired Sky Bow I values not inherited · Warhead mass
Single source90 kg[source]Sky Bow II only; retired Sky Bow I values not inherited
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Unit cost | $165,400[source] | — |
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| Warhead | Annular blast fragmentation warhead, 90 lb (41 kg)[source] | — |
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| Detonation mechanism | Proximity fuzed , expanding rod , with a 27 ft (8.2 m) kill radius[source] | — |
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| Engine | Hercules MK-58 solid-propellant rocket motor[source] | — |
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| Guidance system | Semi-active radar homing[source] | — |
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| Launch platform | Ship, Buk-M1 (modified for use in Ukraine)[source] | Underground silos and mobile launch vehicles[source]Sky Bow II only; retired Sky Bow I values not inherited Towed quad launchers[source]Sky Bow III only; retired Sky Bow I values not inherited |
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| Source measurement | US Navy doctrine stressed long-range air cover to counter both high-speed aircraft and missiles, and development of newer short range defenses had been largely ignored. While the Navy was developing expensive long-range fighters like the Douglas F6D Missileer , most ships were left with older weapons, typically Bofors 40 mm guns or Oerlikon 20 mm cannons . By the early 1960s their capability against modern aircraft and missiles was limited; a lack of fast-reacting mounts, gunsight radars of limited accuracy, and long settling times for the fire control systems all meant that the guns were unlikely to be able to respond effectively against high-speed aircraft.[source]RIM-7 Sea Sparrow · History / Background; only the objects and conditions stated in this passage The Sea Sparrow was far from an ideal weapon. Its rocket engine was designed with the assumption that it would be launched at high speed from an aircraft, and therefore is optimized for a long cruise at relatively low power. In the surface-to-air role one would rather have very high acceleration in order to allow it to intercept sea-skimming targets as soon as possible. The power profile is also suitable for cruising in thin air at high altitudes, but at low altitudes it does not produce enough power to overcome drag and dramatically decreases range; some estimates indicate that the Sea Sparrow may be effective only to 10 kilometres (6.2 mi), about one quarter of the range of the air-launched Sparrow. An engine of much higher power would greatly improve performance, in spite of a shorter burning time.[source]RIM-7 Sea Sparrow · History / Basic point defense missile system (BPDMS); only the objects and conditions stated in this passage IBPDMS emerged as the RIM-7H, which was essentially the RIM-7E with the mid-mounted wings modified to be able to fold. This was done in a fashion similar to carrier-based aircraft; the wings were hinged at a point about 50% along the span, with the outer portions rotated back toward the body of the missile. This allowed them to be stored in tighter container tubes in the new Mark 29 missile launcher , and flip open automatically when they were released from the tube. The other major change was to allow the seeker to work with a variety of illumination radars, including those being used with existing European missile systems.[source]RIM-7 Sea Sparrow · History / Improved basic point defense missile system (IBPDMS); only the objects and conditions stated in this passage Production of the RIM-7H began in 1973 as NATO Sea Sparrow Missile System (NSSMS) Block I. For the US Navy's use the new Mark 95 illuminator system was also introduced, similar to the original Mark 115 but with automatic guidance that could be used in any weather. The Mark 95 formed the basis of the highly automated Mark 91 fire control system.[source]RIM-7 Sea Sparrow · History / Improved basic point defense missile system (IBPDMS); only the objects and conditions stated in this passage In 1972 Raytheon started a Sparrow upgrade program to arm the upcoming F-15 Eagle , producing the AIM-7F. The F model replaced the older analog guidance system with a solid state version that could operate with the F-15's new pulse-doppler radar. The guidance system was much smaller, which allowed the warhead to be moved from its former rear-mounted position to one in front of the mid-mounted wings, and increased in weight to 86 lb (39 kg). Moving it forward also allowed the rocket engine to be enlarged, so it was replaced by a new dual-thrust engine that quickly accelerated the missile to higher speeds, and then settled to a lower thrust for cruise. The new missiles were quickly adapted for the naval role in a fashion similar to the RIM-7H, producing the RIM-7F. The new missile used the lower model designation in spite of the newer technology than the H model.[source]RIM-7 Sea Sparrow · History / Missile upgrades; only the objects and conditions stated in this passage Another major upgrade to the AIM-7 followed, the AIM-7M. The M included a new monopulse radar seeker that allowed it to be shot downward from a higher-altitude aircraft at a target otherwise masked by the ground. The new model also included a completely computerized guidance system that could be updated in the field, as well as further reducing weight for yet another warhead upgrade. The computerized guidance system also included a simple autopilot that allowed the missile to continue flying toward the last known target location even with the loss of a signal, allowing the launch platform to break lock for short periods while the missile was in flight. All of these modifications also improved performance against low-altitude sea-skimming targets as well. The M model entered US operational service in 1983.[source]RIM-7 Sea Sparrow · History / Missile upgrades; only the objects and conditions stated in this passage The original RIM-7E was capable to fly at about Mach 2+, between 30 and 15,000 metres (98 and 49,213 ft), with a range of 15–22 kilometres (8.1–11.9 nmi) (depending on the target height). The RIM-7F enhanced the performances, but also the proximity fuse versus low flying targets, as the minimum altitude was reduced to 15 metres (49 ft) or less. The RIM-7M was able to strike targets at an altitude of 8 metres (26 ft), providing some capability against sea-skimming missiles such the Exocet .[source]RIM-7 Sea Sparrow · History / Missile upgrades; only the objects and conditions stated in this passage Taiwan operates ground based Sea Sparrows as part of the Skyguard SHORAD system. Five hundred missiles entered service in 1991 and are deployed on trailers with four box launchers. In 2012 they were temporarily withdrawn from service following a pair of missile failures during testing as well as the failure of a related AIM-7 in the same exercises.[source]RIM-7 Sea Sparrow · History / Ground-launched Sea Sparrow; only the objects and conditions stated in this passage In January 2023, the United States announced it would transfer Sea Sparrow missiles to Ukraine as part of a military aid package during the 2022 Russian invasion of Ukraine . The Sea Sparrows are fired from Soviet-era 9K37 Buk missile launchers modified by Ukraine to accept them, to counter attacks from cruise missiles and drones. The system, dubbed " FrankenSAM ", utilizes three different air defense missiles—RIM-7 Sea Sparrow missiles, AIM-9 Sidewinder missiles, plus Patriot missiles and Patriot sensor elements —in combination air defense systems based on older Ukrainian tracked vehicles and the Buk missile system. FrankenSAM was confirmed to be in use in December 2023, and was first used successfully in combat to bring down a Russian Shahed drone on 17 January 2024 from 9 km distance.[source]RIM-7 Sea Sparrow · History / Ground-launched Sea Sparrow; only the objects and conditions stated in this passage The ESSM takes the existing guidance section from the RIM-7P and fits it to an entirely new rear-section. The new missile is 10 inches (25 cm) in diameter instead of the previous 8 inches, which allows for a much more powerful motor. It also eliminates the mid-mounted wings entirely, replacing them with long fins similar to those on the Standard missile (and practically every other Navy missile since the 1950s) and moves guidance control to the rear fins. The tail-fin based steering of the ESSM uses up more energy but offers considerably higher maneuverability while the engine is still firing.[source]RIM-7 Sea Sparrow · History / Evolved Sea Sparrow missile (ESSM); only the objects and conditions stated in this passage | — |
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| Used by | — | Military of the Republic of China[source] |
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| Role | — | surface-to-air missile[source]Sky Bow II only; retired Sky Bow I values not inherited surface-to-air missile[source]Sky Bow III only; retired Sky Bow I values not inherited |
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| Propulsion | — | Single-stage dual-thrust solid-fuel rocket motor[source]Sky Bow II only; retired Sky Bow I values not inherited Solid-fuel rocket motor[source]Sky Bow III only; retired Sky Bow I values not inherited |
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| Guidance | — | Inertial with mid-course guidance update from ground-based phased array radar, Active radar homing ( ARH ) for terminal guidance[source]Sky Bow II only; retired Sky Bow I values not inherited |
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| Introduced | — | 1997[source]Sky Bow II only; retired Sky Bow I values not inherited |
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| Country of origin | — | Taiwan[source]Inventory Origin column; table 5, row 4, cell 2; revision 1370505017; retrieved 2026-09-30 |
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