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AH-1Z Viper versus THAAD
Picture Author: Gunnery Sgt. Rome Lazarus

Wikimedia Source: Wikimedia Commons

Main Source: Defense Visual Information Distribution Service - dvidshub.net
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Attack helicopter Type Mobile anti-ballistic missile system
United States of America Place of Origin United States of America
30 September 2010 - present Service Period and Status 2008–present
Designed Period 1987
Unit cost:
US$27 million
US$31 million (new built)
Program & Unit Cost
2000–present Production Period 2008–present
61 Number Built
Bell AH-1 SuperCobra Related Projects
8 December 2000 First Flight
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
58 ft 3 in / 17.8 m Length
14 ft 4 in / 4.37 m Height
2: pilot, co-pilot/gunner (CPG) Crew
6,661 lb / 3,021 kg Payload
2 × General Electric T700-GE-401C turboshaft, 1,800 shp (1,340 kW) each Powerplant
4 blades on main rotor, 4 blades on tail rotor Rotor Systems
48 ft / 14.6 m Rotor Diameter
1,808 ft² / 168.0 m² Disc Area
Never exceed speed:
222 knots / 255 mph / 411 km/h in a dive

Cruise speed:
160 kt / 184 mph / 296 km/h
Speed
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
20,000+ ft / 6,000+ m Service Ceiling
2,790 ft/min / 14.2 m/s Rate of Climb
System Components A THAAD battery consists of:
6 launcher vehicles
2 mobile tactical operations centers (TOCs)
AN/TPY-2 ground-based radar (GBR)
Missiles / Rockets per Launcher 8
Radar Band & Frequency 8.55–10 GHz X band
Search / Detection / Coverage Range Range:
2,900 miles / 4,700 km
Missile / Rocket Mass / Weight 900 kg
Missile / Rocket Length / Height 6.17 m
Missile / Rocket Diameter / Width 34 cm
Missile / Rocket Engine Pratt & Whitney Single-stage rocket
Propellant Solid-fueled rocket
Missile / Rocket Range >200 km
Missile / Rocket Altitude 150 km
Missile / Rocket Speed and Velocity Mach 8.24 / 2.8 km/s
Guidance System Indium-antimonide imaging infra-red seeker head
Launch Platform TEL
The main source of the data presented on this website is en.wikipedia.org.
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