Diamondback (missile)
Encyclopedia
Diamondback was a proposed nuclear-armed air-to-air missile studied by the United States Navy
United States Navy
The United States Navy is the naval warfare service branch of the United States Armed Forces and one of the seven uniformed services of the United States. The U.S. Navy is the largest in the world; its battle fleet tonnage is greater than that of the next 13 largest navies combined. The U.S...

's Naval Ordnance Test Station during the 1950s. Intended as an enlarged, nuclear-armed version of the successful Sidewinder
AIM-9 Sidewinder
The AIM-9 Sidewinder is a heat-seeking, short-range, air-to-air missile carried mostly by fighter aircraft and recently, certain gunship helicopters. The missile entered service with United States Air Force in the early 1950s, and variants and upgrades remain in active service with many air forces...

 missile, Diamondback did not progress beyond the study stage.

Development history

In 1956, studies began at the Naval Ordnance Test Station (NOTS) at China Lake, California
California
California is a state located on the West Coast of the United States. It is by far the most populous U.S. state, and the third-largest by land area...

 involving an advanced development of the AAM-N-7 (later AIM-9) Sidewinder air-to-air missile, which was then entering service with the United States Navy. Originally known as "Super Sidewinder", the program soon gained the name "Diamondback", continuing China Lake's theme of naming heat-seeking missiles after pit vipers.

Diamondback was intended to provide increased speed, range and accuracy over that achieved by Sidewinder. The missile's design called for it to be armed with either a powerful continuous-rod warhead
Continuous-rod warhead
A continuous-rod warhead is a specialized munition that exhibits an annular blast fragmentation pattern. It is used in anti-aircraft and anti-missile missiles.-Early anti-aircraft munitions:...

 or a low-yield nuclear warhead, the latter developed by China Lake's Special Weapons Division, and which would have a yield of less than 1 ktonTNT).

The propulsion system was intended to be a liquid-fueled, dual-thrust
Dual-thrust
In a dual-thrust solid fuel rocket motor, the propellant mass is composed of two different types or densities of fuel. In the case of a tandem dual-thrust motor, the fuel closest to the rocket nozzle burns fast and the fuel further into the motor's body burns slower...

 rocket, using hypergolic, storable propellants. The rocket motor planned for use in the Diamondback missile was based on that developed by NOTS for the Liquid Propellant Aircraft Rocket (LAR) project.

Although the design studies were promising, the Navy did not have a requirement for a missile of this sort. As a result, the Diamondback project was dropped; studies came to a halt around 1958, while by the early 1960s the project was considered "inactive" and was allowed to fade into history.
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