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Contents

   



(Top)
 


1 Development history  





2 Description  





3 Operators  





4 References  














AGM-53 Condor






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AGM-53 Condor
AGM-53 Condor
TypeAir-to-surface guided missile
Place of originUnited States
Production history
ManufacturerRockwell
Specifications
Mass2,100 lb (950 kg)
Length13 feet 10 inches (4.22 m)
Diameter17 inches (43 cm)
Wingspan4 feet 5 inches (1,350 mm)
Warhead630 pounds (290 kg) linear shaped charge warhead or W73 nuclear warhead

EngineRocketdyne MK 70 solid-fuel rocket

Operational
range

60 nmi (69 mi; 110 km)
Maximum speed Mach 2.9

Launch
platform

Aircraft

In 1962, the U.S. Navy issued a requirement for a long-range high-precision air-to-surface missile. The missile, named the AGM-53A Condor, was to use a television guidance system with a data link to the launching aircraft similar to the system of the then projected AGM-62 Walleye.

Development history[edit]

Because of numerous problems in the development phase, the first flight of an XAGM-53A missile did not occur before March 1970.

On 4 February 1971, in its first live warhead test, a Condor made a direct hit on the ex-US navy destroyer escort USS Vammen, while tests later that year demonstrated the ability to hit targets at a range of 30 nmi (35 mi; 56 km).[1] The AGM-53 program was cancelled in March 1976. Its long range and potentially high precision made the Condor a very powerful weapon, but it was much more expensive than contemporary tactical air-to-ground weapons. The secure data link contributed a significant portion to total missile cost, and it certainly didn't help that this link was still somewhat unreliable.

Description[edit]

Diagram of the AGM-53A Condor tactical missile.

The Condor was to be a long-range missile to be used for high-precision stand-off attacks. The missile was launched by the strike aircraft from a distance of up to 60 nautical miles (110 km; 69 mi) to the general target area. When the AGM-53 approached the expected target position, the image of the TV camera in the missile's nose was transmitted back to the operator in the launching aircraft. The operator could switch between wide and narrow field-of-view images to find a suitable target.

As soon as a target for the missile had been selected, the operator could either fly the missile manually until impact, or lock the Condor on the target and rely on the missile's capability to home on the final aiming point. The Condor's linear shaped charge warhead detonated on impact.

A variant of the Condor was anticipated to carry the W73 nuclear warhead, a derivative of the B61 nuclear bomb. Details on the W73 are poorly documented, and it never entered production or service.

Operators[edit]

References[edit]

  1. ^ Pretty 1976, p. 149.

Retrieved from "https://en.wikipedia.org/w/index.php?title=AGM-53_Condor&oldid=1206237271"

Categories: 
Air-to-surface missiles of the United States
Abandoned military rocket and missile projects of the United States
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This page was last edited on 11 February 2024, at 16:02 (UTC).

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