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Matador Liftoff


Specifications

The Matador was the first operational guided missile in use by the U.S.


Wright Air Development Center Digital Collection
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Aircraft - TM-61 Matador (U.S.A.)

The Matador was a surface to surface tactical missile which could carry a conventional or nuclear warhead.  The missile age had started on September 8, 1944 when the first German V-2 missile hit London.  While several attempts at missiles were attempted by the allies, and even a manned missile by he Japanese, the TM-61 Matador was the first operational guided missile in use by the U.S.  The concept was modeled after a German V-1 "buzz bomb" of WWII.  The Matador was launched by a booster rocket from a trailer and was controlled electronically from the ground during flight.  I used a booster rocket to gain altitude, which fell away as the jet engine took over.  There were over one thousand Matador's by 1957, but in 1959 they began to be phased out in favor of the more advanced Martin Mace.

"In July 1949, the Matador and Firebird missiles were canceled and other missile projects were downgraded to component developments or studies, or were canceled altogether.  The Soviets' first atomic bomb test in August shook U.S. complacency but failed to generate progress in the missile program.  At the start of the Korean War, the Air Force had only three missiles in development: Navaho, Rascal, and Falcon."

"...in January 1952, when the Air Force ... had to prevail upon Secretary of the Air Force Finletter not to cancel the Matador short-range (100-500 miles) missile, because the Army was certain to claim it or the close air support mission as a consequence."

-Source Ballistic Missiles in the United States Air Force 1945-1960 by Jacob Neufeld, Office of Air Force History 1990.

Matador

Specifications of theTM-61 Matador

Span: 27 ft. 11 in.

Length: 39 ft. 8 in.

Height: 9 ft. 8 in.

Weight: 13,593 lbs. at launch

Armament: Conventional or nuclear warhead

Engine: Allison J33 of 4,600 lbs. thrust; Aerojet solid-propellant booster rocket of 57,000 lbs. thrust

Cost: $132,000

PERFORMANCE

Max. speed: 600 mph/521 knots in level flight; supersonic during final dive

Range: 690 statute miles/600 nautical miles

Service ceiling: 44,000 ft.

Source: U.S. Air Force History Museum

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