Diamondback (missile)
| Diamondback | |
|---|---|
 | |
| Type | Air-to-air missile |
| Place of origin | United States |
| Service history | |
| Used by | United States Navy |
| Production history | |
| Designed | 1956-1957 |
| Manufacturer | Naval Ordnance Test Station |
| No. built | 0 |
| Specifications | |
| Mass | 850 pounds (390 kg) |
| Length | 12.3 feet (3.76 m) |
| Diameter | 12 inches (300 mm) |
| Wingspan | 40 inches (1,000 mm) |
| Warhead | Nuclear warhead |
| Blast yield | 0.75 kilotons of TNT (3.1 TJ) |
| Engine | Dual-thrust rocket |
| Propellant | Liquid fuel UDMH/RFNA |
Operational range | 15 to 20 miles (24 to 32 km) |
| Flight ceiling | 80,000 feet (24,000 m) |
| Maximum speed | Mach 3+ |
Guidance system | Infrared seeker/passive radar guidance |
The Diamondback was a proposed nuclear-armed air-to-air missile studied by the United States Navy's Naval Ordnance Test Station during the 1950s. Intended as an enlarged, nuclear-armed version of the successful Sidewinder missile, Diamondback did not progress beyond the study stage.
Development history
[edit]In 1956, studies began at the Naval Ordnance Test Station (NOTS) at China Lake, California 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.[1][2]
Diamondback was intended to provide increased speed, range and accuracy over that achieved by Sidewinder.[3][4] The missile's design called for it to be armed with either a powerful continuous-rod warhead or a low-yield nuclear warhead,[5] the latter developed by China Lake's Special Weapons Division, and which would have a yield of less than 1 kiloton of TNT (4.2 TJ).[6]
The propulsion system was intended to be a liquid-fueled, dual-thrust rocket,[5] using hypergolic, storable propellants.[7] 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.[8]
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,[1] while by the early 1960s the project was considered "inactive" and was allowed to fade into history.[3][5]
References
[edit]Notes
[edit]Bibliography
[edit]- Babcock, Elizabeth (2008). Magnificent Mavericks: transition of the Naval Ordnance Test Station from rocket station to research, development, test and evaluation center, 1948–58. History of the Navy at China Lake, California. Vol. 3. Washington, DC: Government Printing Office. ISBN 978-0-945274-56-8. Retrieved 2011-01-13.
- Besserer, C.W.; Hazel C. Besserer (1959). Guide to the Space Age. Englewood Cliffs. NJ: Prentice-Hall. ASIN B004BIGGO6.
- Bowman, Norman John (1957). The Handbook of Rockets and Guided Missiles. Chicago: Perastadion Press. ASIN B002C3SPN2. Retrieved 2011-01-13.
- Jacobs, Horace; Eunice Engelke Whitney (1962). Missile and Space Projects Guide: 1962. New York: Plenum Press. ASIN B0007E2BBK.
- Parsch, Andreas (2024). "(Other): "Missile Scrapbook"". Directory of U.S. Military Rockets and Missiles. designation-systems.net. Retrieved 2011-01-13.