F-4E Phantom II
Country of Origin: United StatesImage courtesy of the United States Air Force; click on image to display larger version
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F-4E Phantom IICountry of Origin: United StatesImage courtesy of the United States Air Force; click on image to display larger version |
| Specifications | |
| Type: Two-seat interceptor/fighter | Manufacturer: McDonnell-Douglas |
| Armor Material: Steel, aluminum, titanium in certain sections | Armor Thickness: n/a |
| Length: 19.2 m | Wingspan: 11.7 m |
| Weight: 28,030 kg (max takeoff weight) | Maximum Speed: 2400 kph (on afterburner) |
| Powerplant: 2 x General Electric J79-GE-17A turbojets | Thrust: 8117 kg each |
| Description | |
| Size: 10 | Total Actions: 2 |
| Offense | |||||||||||||
| Weapon | Code | Arc | S | M | L | EX | Acc | FC | Dam | Qty | ROF | Special | Ammo |
| M61A1 20mm autocannon | LAAC | FF | 2 | 4 | 8 | 16 | 0 | 0 | x8 | 1 | +6 | - | 639 |
| AIM-7M Sparrow | AAM | FF | 20 | 40 | 80 | 160 | -1 | 0 | x14 | 1 | 0 | Guided, Seeking (2) | 4 |
| AIM-9 Sidewinder | AAM | FF | 8 | 16 | 32 | 64 | +1 | 0 | x10 | 1 | 0 | Guided, Min Range 10 | 4 |
| Total of 5 available external hardpoints (use per rules in Technical Manual Second Edition, p. 149 and Banzaidyne New Perks and Flaws) | |||||||||||||
| Defense | |
| Primary Movement: Flight 8/31/80 (2400 kph) | Secondary Movement: Ground 20/40 (240 kph) |
| Maneuver: -1 | Armor: 11 / 22 / 33 |
| Miscellaneous | |
| Crew: 2 (Pilot, Weapons Systems Officer) | Deployment Range: 1400 km |
| Sensors: 0 / 3 km ground, 30 km air | Communications: 0 / 20 km ground, 200 km air |
| Perks: Autopilot (AUX), Backup Communications, Catapult Hook (AUX), Chaff/Flare Dispensers (AUX, Rating 2, 30 shots), Ejection System (AUX), Refueling Intake, Reinforced Chassis, Stratospheric Flight (ceiling: 18.3 km) | Flaws: Decreased Maneuverability (SMS, Rating 1), Requires Airstrip, Traceable Emissions (smoky engines, Rating 1) |
| Defects: None | Lemon Dice: 2 |