| Hopi | |
|---|---|
&sq=Qlik&lang=&file=File:Hopi_on_AD-5N.jpg) Hopi mounted on an AD-5N Skyraider | |
| Type | Air-to-surface missile |
| Place of origin | United States |
| Service history | |
| Used by | United States Navy |
| Production history | |
| Designed | Mid-to-late 1950s |
| Manufacturer | Naval Ordnance Test Station |
| Specifications | |
| Warhead | W50 thermonuclear |
| Blast yield | 60 to 400 kilotonnes of TNT (250 to 1,670 TJ) |
| Engine | Solid-fuel rocket |
The Hopi was an air-to-surface missile developed by the United States Navy's Naval Ordnance Test Station. Intended to provide a medium-range nuclear capability for carrier aircraft, the missile reached the flight test stage during 1958, but the project was cancelled following testing and no production was undertaken.