MiG-23ML "Flogger-G"
Country of Origin: former Soviet UnionImage courtesy of the U.S. Department of Defense; click on image to display larger version
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MiG-23ML "Flogger-G"Country of Origin: former Soviet UnionImage courtesy of the U.S. Department of Defense; click on image to display larger version |
| Specifications | |
| Type: Single-seat interceptor | Manufacturer: Mikoyan-Gurevich |
| Armor Material: n/a | Armor Thickness: n/a |
| Length: 16.6 m | Wingspan: 13.96 m (wings spread), 7.78 m (wings swept) |
| Weight: 17,800 kg (max takeoff weight) | Maximum Speed: 1885 kph |
| Powerplant: Turmansky R-35-300 afterburning turbojet | Thrust: 8548 kg dry, 12,998 kg on afterburner |
| Description | |
| Size: 9 | Total Actions: 1 |
| Offense | |||||||||||||
| Weapon | Code | Arc | S | M | L | EX | Acc | FC | Dam | Qty | ROF | Special | Ammo |
| GSh-23L 23mm autocannon | LAC | FF | 2 | 4 | 8 | 16 | 0 | -1 | x8 | 1 | +2 | - | 260 |
| Total of 6 available external hardpoints (use per rules in Technical Manual Second Edition, p. 149 and Banzaidyne New Perks and Flaws) | |||||||||||||
| Defense | |
| Primary Movement: Flight 8/40/83 (2490 kph) | Secondary Movement: 20/40 (240 kph) |
| Maneuver: -1 | Armor: 10 / 20 / 30 |
| Miscellaneous | |
| Crew: 1 (Pilot) | Deployment Range: 1950 km |
| Sensors: -1 / 3 km ground, 30 km air | Communications: -1 / 10 km ground, 100 km air |
| Perks: Autopilot (AUX), Backup Communications, Ejection System (AUX), Stratospheric Flight (ceiling: 18.5 km) | Flaws: Decreased Maneuverability (SMS, Rating 1), Requires Airstrip |
| Defects: None | Lemon Dice: 2 |