McDonnell Douglas F-4G Phantom II Aircraft Data
The McDonnell Douglas F-4G is a modified version of the F-4E, tailored to the suppression of enemy air-defense (SEAD) role. The biggest change to the E_Model F-4 was the installation of the APR-38 'RHAW' mission electronics package. The RHAW's senors completely occupy the redesigned nose, forsaking the M61A1 Gatling gun. The back-seater's cockpit is missionized with dedicated controls. The centerline pylon is strengthed to accept the 600l drop-tank from the F-15.
The outer-wing pylons, which normally carry drop-tanks, have been rewired to carry the AGM-88 High-speed Anti-Radiation Missile (HARM). The standard fit of USAF Mk.82/84 bombs along with CBU munitions. The F-4G flew in the 1991 Gulf War with one loss due to enemy fire. F-4G's from the 190th Squadron, Idaho ANG were the last Phantoms to fly in USAF service. The F-4G modification was never exported outside of the U.S.
The outer-wing pylons, which normally carry drop-tanks, have been rewired to carry the AGM-88 High-speed Anti-Radiation Missile (HARM). The standard fit of USAF Mk.82/84 bombs along with CBU munitions. The F-4G flew in the 1991 Gulf War with one loss due to enemy fire. F-4G's from the 190th Squadron, Idaho ANG were the last Phantoms to fly in USAF service. The F-4G modification was never exported outside of the U.S.
- Country of Origin: United States
- First Flight: 1975
- Initial Service Date: 1978
- No. Built: 134
- No. In Service: 0
- No. of Hardpoints: 9
- Crew: 2
Power:
2 × General Electric J79-GE-17 axial compressor turbojets at 79.5 kN
Weapons:
Mk. 82 500lb bombs.
CBU-52 cluster bomb units.
AGM-65A/B/D 'Maverick' missiles.
AGM-88A HARM missiles
AIM-7F 'Sparrow' missiles.
AIM-9L 'Sidewinder' missiles.
CBU-52 cluster bomb units.
AGM-65A/B/D 'Maverick' missiles.
AGM-88A HARM missiles
AIM-7F 'Sparrow' missiles.
AIM-9L 'Sidewinder' missiles.
Dimensions:
| Length: | 19.20 m. |
| Wing Span: | 11.68 m. |
| Wing Area: | 49.2 m² |
| Height: | 5.03 m. |
| Empty Weight: | 13,770 kg. |
| Max. Weight: | 27,965 kg. |
| Max. Ordnance Load: | 2,268 kg. |
Performance:
| Max. Speed: | 2,390 kph |
| Cruise Speed: | 940 kph |
| Service Ceiling: | 18,288 m. |
| Normal Range: | 1,300 km |
| Max. Range: | 2,600 km |
Random great photos of the McDonnell Douglas F-4G Phantom II:
