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THAAD versus Leclerc
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Picture Author: Pierre-Yves Beaudouin / Wikimedia Commons / CC BY-SA 4.0

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Mobile anti-ballistic missile system Type Main battle tank
United States of America Place of Origin France
2008–present Service Period and Status 1993–present
1987 Designed Period 1983–1989
Program & Unit Cost Unit cost
₣rs 104,304,000 in 1993, US $4+ million in 2016
2008–present Production Period 1990–2008 (The last unit was produced in 2007 and the production line was closed, although Nexter retains the capability to build more if there is a need)
Number Built ~862
Mass / Weight / Displacement series 1: 54.5 tonnes
series 2: 56.3 tonnes
series XXI : 57.4 tonnes
Length 9.87 m (6.88 without gun)
Width / Beam 3.60 m
Height 2.53 m
Crew 3 (Commander, gunner, driver)
Fuel Capacity 1300 litres (1700 with fuel drums)
Speed 72 km/h (45 mph) on the road
55 km/h (34 mph) on all-terrains
Operational Range 550 km
650 km (400 mi) with external fuel
Power-to-Weight Ratio 27.52 hp/tonne
Armament Main armament: GIAT CN120-26/52 120mm tank gun
40 rounds (1 round ready to fire in the chamber, 22 rounds inside the autoloader magazine with additional 18 rounds cylinder in the hull)
Secondary armament:
12.7 mm coaxial M2HB machine gun (1,100 rounds)
7.62 mm machine gun (3,000 rounds)
Armor modular composite armor
SXXI version include titanium, tungsten and semi-reactive layers
Engine 1,100 kW (1,500 hp) V8X SACM (Wärtsilä) 8-cylinder diesel engine
Transmission Automatic SESM
Suspension hydropneumatic
A THAAD battery consists of:
6 launcher vehicles
2 mobile tactical operations centers (TOCs)
AN/TPY-2 ground-based radar (GBR)
System Components
8 Missiles / Rockets per Launcher
8.55–10 GHz X band Radar Band & Frequency
Range:
2,900 miles / 4,700 km
Search / Detection / Coverage Range
900 kg Missile / Rocket Mass / Weight
6.17 m Missile / Rocket Length / Height
34 cm Missile / Rocket Diameter / Width
Pratt & Whitney Single-stage rocket Missile / Rocket Engine
Solid-fueled rocket Propellant
>200 km Missile / Rocket Range
150 km Missile / Rocket Altitude
Mach 8.24 / 2.8 km/s Missile / Rocket Speed and Velocity
Indium-antimonide imaging infra-red seeker head Guidance System
TEL Launch Platform
The main source of the data presented on this website is en.wikipedia.org.
All photos uploaded on this website are from commons.wikimedia.org.