Directory of U.S. Military Rockets and Missiles
Appendix 4: Undesignated Vehicles
Copyright © 2003-2009 Andreas Parsch

Lockheed Martin THAAD

The THAAD (Terminal High Altitude Area Defense - originally "Theater High Altitude Area Defense", renamed in Feb. 2004) missile defense system was first proposed in 1987, and in 1990 the formal request for proposals was submitted to the industry. In September 1992, the U.S. Army selected Lockheed Martin as prime contractor for THAAD development, and the first THAAD flight test occurred in April 1995.

A THAAD battery consists of about nine launch trucks with ten missiles each, two mobile tactical operations centers, and the Ground-Based Radar (GBR). The GBR is employed for surveillance at ranges of up to 1000 km (600 miles), target identification and target tracking. Targeting information is uploaded to the missile immediately before launch and continuously updated during the flight. The THAAD missile is powered by a single stage solid-propellant rocket motor with thrust vectoring. After burnout, the booster is separated from the kill vehicle (KV), which continues to the interception point. For exo-atmospheric manoeuvering, the KV is equipped with a Boeing-developed liquid DACS (Divert and Attitude Control System). In the terminal intercept phase, the KV is guided by an InSb staring FPA (Focal Plane Array) infrared seeker, whose window is protected in the initial flight phase by a clamshell protection shroud. The KV has no explosive warhead and destroys the target by direct impact. The THAAD can intercept ballistic missile targets at altitudes up to 150 km (93 miles) at a range of more than 200 km (125 miles).

Photo: U.S. Army

Between 21 April 1995 and 2 August 1999, a total of 11 THAAD flight tests occurred. The initial tests validated propulsion and seeker systems, and the first actual intercept was attempted in the 4th flight on 13 December 1995. However, the test failed and the first successful interception (a Hera ballistic target) actually did not occur before the 10th flight on 10 June 1999! The reasons for the preceding six failures were various, and included failures in the propulsion system, stage separation, seeker soft- and hardware, and the kill vehicle's DACS. The 11th test was also successful, but the system's bad test record of course significantly delayed the program.

Photo: U.S. Army
THAAD Launcher

In late 1999, it was decided to enter the EMD (Engineering and Manufacturing Development) phase of the THAAD program, and the EMD contract was awarded to Lockheed Martin in June 2000. The first EMD flight test occurred on 22 November 2005, and tested missile launch, flight control, and KV separation and control, but did not involve an actual target. Until March 2009, a total of 11 THAAD tests, including six actual intercepts, had been conducted, all of which were successful.

In January 2007, Lockheed Martin received the first production contract for THAAD, covering 48 missiles, six launchers and two fire control and communications units. In May 2008, the Army's first THAAD battery was formally activated. The U.S. Army plans to procure more than 1400 THAAD missiles, which will eventually form the upper-tier complement to the Patriot PAC-3 in the Army's TBMD (Theater Ballistic Missile Defense) system.


Note: Data given by several sources show slight variations. Figures given below may therefore be inaccurate!

Data for THAAD:

Length6.17 m (20 ft 3 in)
Diameterbooster: 34 cm (13.4 in); KV: 37 cm (14.5 in)
Weight900 kg (2000 lb)
Speed2800 m/s (9200 fps)
Ceiling150 km (93 miles)
Range> 200 km (125 miles)
PropulsionPratt & Whitney solid-fueled rocket
Warheadnone ("hit-to-kill")

Main Sources

[1] Hajime Ozu: "Missile 2000 - Reference Guide to World Missile Systems", Shinkigensha, 2000
[2] Lockheed Martin Missiles and Fire Control Website
[3] Website
[4] Army Technology Website: "THAAD Theater High Altitude Area Defense Missile System", Net Resources International Ltd.
[5] Center for Defense Information Website

Back to Directory of U.S. Military Rockets and Missiles, Appendix 4

Last Updated: 25 June 2009