AIM-54_Phoenix
Tempat asal | Amerika Syarikat |
---|---|
Dihasilkan | 1966 |
Sistempemanduan | Semi-active and active radar homing |
Dalam perkhidmatan | 1974–2004 |
Detonationmechanism | Proximity fuze |
Kelajuan | Mach 5[1] |
Lebar sayap | 3 ka (910 mm) |
Warhead | 135 lb (61 kg), high explosive |
Berat | 1,000–1,040 lb (450–470 kg) |
Panjang | 13 ka (4.0 m) |
Altitud penerbangan | 80,000 ka (24 km) |
Enjin | Solid propellant rocket motor |
Digunakan oleh | United States Navy (former) Iranian Air Force |
Kos unit | AS$477,131 |
Siling penerbangan | 100,000 ka (30 km) |
Jarakoperasi | 100 nmi (190 km) |
Pengeluar | Hughes Aircraft Company Raytheon Corporation |
Diameter | 15 in (380 mm) |
Platformpelancaran | Grumman F-14 Tomcat General Dynamics-Grumman F-111B |
Jenis | Peluru berpandu udara ke udara jarak jauh |