F/A-18C Hornet
Country of Origin: United StatesImage courtesy of the United States Navy; click on image to display larger version
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F/A-18C HornetCountry of Origin: United StatesImage courtesy of the United States Navy; click on image to display larger version |
| Specifications | |
| Type: Light tactical fighter | Manufacturer: Boeing (formerly McDonnell Douglas) |
| Armor Material: Aluminum, titanium, carbon/epoxy | Armor Thickness: n/a |
| Length: 17.07 m | Wingspan: 12.32 m (over wingtip Sidewinder missiles) |
| Weight: 22,328 kg (max takeoff weight in attack configuration) | Maximum Speed: 2220 kph |
| Powerplant: 2 x General Electric F404-GE-400 turbofans with afterburners | Thrust: 7,257 kg each with afterburner |
| Description | |
| Size: 9 | Total Actions: 2 |
| Offense | |||||||||||||
| Weapon | Code | Arc | S | M | L | EX | Acc | FC | Dam | Qty | ROF | Special | Ammo |
| M61A1 6-bbl 20mm Vulcan autocannon | LAAC | FF | 2 | 4 | 8 | 16 | 0 | +1 | x8 | 1 | +6 | - | 515 |
| AIM-9 Sidewinder | AAM | F | 8 | 16 | 32 | 64 | +1 | +1 | x10 | 1 | 0 | Guided, Min Range 10 | 2 |
| Total of 7 available external hardpoints (use per rules in Technical Manual Second Edition, p. 149 and Banzaidyne New Perks and Flaws) | |||||||||||||
| Defense | |
| Primary Movement: Flight 8/37/74 (2220 kph) | Secondary Movement: Ground 23/45 (270 kph) |
| Maneuver: +1 | Armor: 10 / 20 / 30 |
| Miscellaneous | |
| Crew: 1 (Pilot) | Deployment Range: 2000 km |
| Sensors: +2 / 4 km ground, 40 km air | Communications: +1 / 20 km ground, 200 km air |
| Perks: Acceleration Protection, Advanced Controls, Autopilot (AUX), Backup Communications, Catapult Hook (AUX), Chaff/Flare Dispensers (AUX, Rating 2, 60 shots), Ejection System (AUX), Refueling Intake, Stratospheric Flight | Flaws: Decreased Maneuverability (SMS, Rating 2), Requires Airstrip |
| Defects: None | Lemon Dice: 3 |