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Attack helicopter |
Type |
Mobile anti-ballistic missile system |
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30 September 2010 - present |
Service Period and Status |
2008–present |
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Unit cost:
US$27 million
US$31 million (new built) |
Program & Unit Cost |
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2000–present |
Production Period |
2008–present |
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Bell AH-1 SuperCobra |
Related Projects |
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8 December 2000 |
First Flight |
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Empty weight:
12,300 lb / 5,580 kg
Useful load:
5,764 lb / 2,620 kg
Max. takeoff weight:
18,500 lb / 8,390 kg |
Mass / Weight / Displacement |
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58 ft 3 in / 17.8 m |
Length |
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14 ft 4 in / 4.37 m |
Height |
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2: pilot, co-pilot/gunner (CPG) |
Crew |
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6,661 lb / 3,021 kg |
Payload |
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2 × General Electric T700-GE-401C turboshaft, 1,800 shp (1,340 kW) each |
Powerplant |
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4 blades on main rotor, 4 blades on tail rotor |
Rotor Systems |
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48 ft / 14.6 m |
Rotor Diameter |
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1,808 ft² / 168.0 m² |
Disc Area |
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Never exceed speed:
222 knots / 255 mph / 411 km/h in a dive
Cruise speed:
160 kt / 184 mph / 296 km/h |
Speed |
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Range:
370 nmi / 426 mi / 685 km
Combat radius:
125 nmi / 144 mi / 231 km with 2,500 lb (1,130 kg) payload |
Operational Range |
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20,000+ ft / 6,000+ m |
Service Ceiling |
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2,790 ft/min / 14.2 m/s |
Rate of Climb |
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System Components |
A THAAD battery consists of:
6 launcher vehicles
2 mobile tactical operations centers (TOCs)
AN/TPY-2 ground-based radar (GBR) |
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Missiles / Rockets per Launcher |
8 |
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Radar Band & Frequency |
8.55–10 GHz X band |
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Search / Detection / Coverage Range |
Range:
2,900 miles / 4,700 km |
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Missile / Rocket Mass / Weight |
900 kg |
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Missile / Rocket Length / Height |
6.17 m |
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Missile / Rocket Diameter / Width |
34 cm |
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Missile / Rocket Engine |
Pratt & Whitney Single-stage rocket |
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Propellant |
Solid-fueled rocket |
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Missile / Rocket Range |
>200 km |
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Missile / Rocket Altitude |
150 km |
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Missile / Rocket Speed and Velocity |
Mach 8.24 / 2.8 km/s |
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Guidance System |
Indium-antimonide imaging infra-red seeker head |
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