| AAM-N-10 Eagle | |
|---|---|
 | |
| Type | Long-range Air-to-air missile |
| Place of origin | United States |
| Service history | |
| Used by | United States Navy |
| Production history | |
| Designed | 1958 |
| Manufacturer | Bendix Corporation |
| No. built | 0 |
| Specifications (projected) | |
| Mass | 650 lb (290 kg) without booster 1,284 lb (582 kg) with booster |
| Length | 11 ft 7 in (3.53 m) without booster 16 ft 1.5 in (4.915 m) with booster |
| Diameter | 14 in (360 mm) booster 16 in (410 mm) |
| Wingspan | 2 ft 10 in (0.86 m) booster 4 ft 2.1 in (1.273 m) folding |
Operational range | 110 nmi (130 mi; 200 km) powered 160 nmi (180 mi; 300 km) aerodynamic |
| Flight ceiling | 100,000 ft (30,000 m) |
| Maximum speed | Mach 4.5 |
Guidance system | inertial with radio correction midcourse active radar or home-on-jam terminal |
| References | Parsch 2003 |
The AAM-N-10 Eagle was a long-range air-to-air missile developed by the Bendix Corporation for use by the United States Navy. Intended for carriage by the Douglas F6D Missileer fleet defense fighter, the Eagle program was cancelled before testing could begin, but the lessons learned were used in the development of the AIM-54 Phoenix missile.