The F-4E variant is basiclly Is just my F-4N that i modified
WIKI
The McDonnell Douglas F-4 Phantom II variants were numerous versions and designations of the F-4 and are described below.
USAF version with an integral M61 Vulcan cannon in the elongated RF-4C nose, AN/APQ-120 radar with smaller cross-section to accommodate the cannon, J79-GE-17 engines with 17,900 lbf (79.379 kN) of afterburner thrust each. Late-series aircraft equipped with leading-edge slats to improve maneuverability at the expense of top speed under the Agile Eagle program. Starting with Block 53, aircraft added AGM-65 Maverick capability and smokeless J79-GE-17C or -17E engines. First flight 1 August 1965. The most numerous Phantom variant; 1,370 built.
Specifications
Spotlights
- TheCommentaryGuy 2.5 years ago
General Characteristics
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- Wingspan 40.9ft (12.5m)
- Length 66.2ft (20.2m)
- Height 17.0ft (5.2m)
- Empty Weight 30,457lbs (13,815kg)
- Loaded Weight 43,610lbs (19,781kg)
Performance
- Power/Weight Ratio 3.246
- Wing Loading 75.1lbs/ft2 (366.6kg/m2)
- Wing Area 580.9ft2 (54.0m2)
- Drag Points 7442
Parts
- Number of Parts 493
- Control Surfaces 5
- Performance Cost 2,259