Skybolt (missile): Difference between revisions
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[[Category:Tír Glas]] | [[Category:Tír Glas]] | ||
{{Infobox weapon | {{Infobox weapon | ||
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==Foreign developments== | ==Foreign developments== | ||
===Socialist Republic of Menghe=== | ===Socialist Republic of Menghe=== | ||
In 1992, Tír Glas issued [[Menghe]] a production license for a composite Skybolt design. This export model had solid-state electronics in the guidance system, but retained the SARH seeker head and heavier fins of the Skybolt IA. As on the Skybolt IA, it had a 45-kilometer range and a 39 kg fragmentation warhead. | |||
Within Menghe, this missile was designated '''YGG-6''' (6식 공대공 유도탄 / 六式空對空誘導彈, ryuk-sik gongdaegong yudotan, "Type 6 air-to-air missile"). On entering service, it was integrated with the [[Daesŭngri DS-5|DS-5M]] and [[Songrim SR-7|SR-7G1]] fighters, and it was later integrated onto the SR-8, SR-9, and DS-10. Though less capable than contemporary Skybolt models, it was a generational leap over the preceding {{wp|R-23 (missile)|YGG-3}}, and was well-received by Menghean pilots. | |||
The YGG-6 served as the basis for the development of the [[YGG-7 Hwasal]], which incorporated an active radar seeker, a dual-pulse motor, and a mid-course datalink. Despite initial rumors that the Hwasal used Skybolt II's seeker head, the seeker and control surfaces were of domestic Menghean design. | |||
===Tír Tairngire=== | ===Tír Tairngire=== | ||
Latest revision as of 22:20, 1 November 2020
Skybolt | |
---|---|
Type | Medium-range, Semi-Active Homing air-to-air missile |
Place of origin | Tír Glas |
Service history | |
In service | 1972 – present |
Used by | See operators |
Production history | |
Manufacturer | • XYZ: 1968–94 • GAIA: 1994–present |
Produced | 1968-1991 |
Variants | Skybolt I, IA, II, III, IIIA, Skybolt 90 |
Specifications | |
Weight | 510 lb (230 kg) |
Length | 12 ft (3.7 m) |
Diameter | 8 in (200 mm) |
Warhead | High explosive blast-fragmentation
• Skybolt I, 66 pounds (30 kg) |
Detonation mechanism | Proximity/impact Fuze |
Engine | Solid-fuel rocket motor |
Wingspan | 42 in (1,100 mm) Skybolt I and II |
Operational range | • Skybolt I: 45 km (24 nmi) • Skybolt II: 60 km (32 nmi) • Skybolt III: 75 km (>38 nmi) |
Speed | Mach 4 (4,900 km/h; 3,045 mph) |
Guidance system | • Skybolt I Semi-active radar homing • Skybolt II and III Inertial guidance Mid-course update Active radar homing |
The Skybolt is a medium-range air to air missile derived from the Dayanese Sparrow missile. In use since the 1970s little of the basic design remains in the variants still fielded.
Skybolt was initially simply to replace the seeker for the Sparrow with a Brennan-Brown semi-active monopulse seeker, this soon developed into a more involved set of changes including the substitution of Dayanese avionics with systems from Collins and the replacement of the fuzing system with a Foley-designed radar-fuze. Monopulse seekers are more accurate, less susceptible to jamming and better able to discriminate targets from ground clutter at lower altitudes. The BB seeker offered significantly better performance than the original seeker allowing XYZ initially to dispense with warhead improvements carried out by Dayashina to address a lack of accuracy.
Skybolt was tested in Dayashina against domestically produced monopulse-equipped Sparrows, In the end the Dayanese elected to use a different seeker than Skybolt for their later marques of Sparrow. Skybolt would go through a variety of upgrades before in the 1990s being supplanted by the lighter but more capable Black Spear also designed by XYZ.
History and development
Skybolt came about from a Glasic plan to fit an inverse monopulse seeker to the Red Top missile in the abortive Blue Dolphin which left a requirement still to be fulfilled. Various options were studied with the Dayanese Sparrow being the preferred choice and by 1968 test firings of the missile were taking place. Major differences between Sparrow and Skybolt were the addition of the monopulse seeker, improved electronics and avionics, improved control surfaces an active-radar fuze and modified rocket motor essentially making the Skybolt a new missile.
Test firings showed that the Skybolt could function properly in a high-ECM environment at both high and low altitude, it could be launched from as low as 100m to attack higher-altitude targets or from higher altitude at targets as low as 75m. The missile entered ARTG and CRTG service in 1972, by this time featuring a dual-pulse motor and larger 39kg warhead.
By 1985 Skybolt II was about to enter service which provided a step change in capability from previous iterations of the missile in that it featured solid-state electronics throughout, an active-homing seeker with inertial mid-course guidance a tapered boat-tail fuselage, thinner control surfaces with electronic actuation and a larger rocket motor. Events would overtake Skybolt II with Skybolt III taking its place. This had all the aforementioned improvements afforded by Skybolt II but also included the deletion of the mid-body fins, further improvements to the electronics and avionics as well as slightly a slightly larger warhead and rocket motor made possible by the deletion of the mid-body fins and shrunken electronics package. This would be the penultimate Skybolt in service with an improved Skybolt III adding thrust-vectoring, an mmW seeker and better ECCM capabilities to the missile. Skybolt 90 would have improved on this further with a dual-seeker and further ECM hardening but development shifted toward a new missile which would become Black Spear.
In 2002 the ARTG announced the launch of the Capability Upgrade and Sustainment Programme or CUSP which replaced obsolete and out-of-production subsystems of Skybolt with those from Black Spear essentially providing the missile with a life-extension into the 2010s.
Variants
Skybolt I | Skybolt IA | Skybolt II | Skybolt IIA | Skybolt III | Skybolt 90 | |
Length | 3.7 m (12.1ft) | 3.68 m (12ft) | 3.66 m (12ft) | |||
Wingspan | 1.02 m (3.3ft) | - | ||||
Finspan | 0.77 m (1.9ft) | |||||
Diameter | 0.210 m (8.2in) | |||||
Weight | 200kg (441lbs) | 230kg (507lbs) | 225kg (496lbs) | |||
Speed | Mach 4 | Mach 4.5 | ||||
Range | 30km (16.1 nmi) | 45km (24.2 nmi) | 60km (32.3 nmi) | 70km (37.8 nmi) | ||
Propulsion | HAJ Swift boost-glide motor | HAJ Swallow dual-pulse motor | HAJ Skylark multi-pulse motor | |||
Warhead | 30kg (66lbs) Continuous Rod | 39kg (86lbs) Fragmentation | 40kg (88lbs) Fragmentation |
Foreign developments
Socialist Republic of Menghe
In 1992, Tír Glas issued Menghe a production license for a composite Skybolt design. This export model had solid-state electronics in the guidance system, but retained the SARH seeker head and heavier fins of the Skybolt IA. As on the Skybolt IA, it had a 45-kilometer range and a 39 kg fragmentation warhead.
Within Menghe, this missile was designated YGG-6 (6식 공대공 유도탄 / 六式空對空誘導彈, ryuk-sik gongdaegong yudotan, "Type 6 air-to-air missile"). On entering service, it was integrated with the DS-5M and SR-7G1 fighters, and it was later integrated onto the SR-8, SR-9, and DS-10. Though less capable than contemporary Skybolt models, it was a generational leap over the preceding YGG-3, and was well-received by Menghean pilots.
The YGG-6 served as the basis for the development of the YGG-7 Hwasal, which incorporated an active radar seeker, a dual-pulse motor, and a mid-course datalink. Despite initial rumors that the Hwasal used Skybolt II's seeker head, the seeker and control surfaces were of domestic Menghean design.
Tír Tairngire
Operators
Current Operators
- Royal Glasic Air Force (ARTG)
- Royal Glasic Navy (CRTG)
- Royal Tairngiric Air Force (ARTT)
Former Operators
- Royal Crainnic Navy (CRTC)
- Royal Ealgan Air Force (ARTE)
- Royal Ealgan Navy (CRTE)
- Royal Tairngiric Navy (CRTT)