ASALM | |
---|---|
Type | High supersonic Air-launched cruise missile |
Place of origin | United States |
Service history | |
Used by | United States Air Force |
Specifications | |
Mass | 2,700 pounds (1,200 kg) |
Length | 14 feet (4.3 m) |
Warhead | W69 thermonuclear |
Blast yield | 200 kilotonnes of TNT (840 TJ) |
Engine | Marquardt rocket/ramjet |
Operational range | 300 miles (480 km) |
Maximum speed | Mach 4.5+, test-flown to Mach 5.5 [1] |
Guidance system | Inertial + passive antiradiation and active radar homing for air-to-air mode[2] |
The Advanced Strategic Air-Launched Missile (ASALM) was a medium-range strategic missile program, developed in the late 1970s for the United States Air Force. Intended for use in both the air-to-surface and anti-AWACS roles, the missile's development reached the stage of propulsion-system tests before being cancelled in 1980.