F/A-14
Revision as of 16:19, 3 September 2016 by o>Ayzek (1 revision imported)
F/A-14 | |
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Role | |
Manufacturer | Høiland Aerospace Incorporated |
Introduction | 1531 |
Retired | n/a |
Status | operational |
Produced | ### |
The F/A-14 is a family of 2-engines, variable-sweep wing combat aircraft which were developed by Høiland Aerospace Incorporated for the Armed Forces of the Imperial Republic of Drahen. Having developed into a multirole aircraft, the F/A-14 is capable of undertaking more mission profiles than just the original strike mission; Drahen replaced multiple aircraft types with the F/A-14 as a common type phasing out many dedicated single role aircraft for specialist purposes such as battlefield reconnaissance, maritime patrol duties, or dedicated electronic countermeasures (ECM).
Design
Variants
- F/A-14 IDS- (interdictor/strike) fighter-bomber
- F/A-14 IDS-2- updated F/A-14 IDS with uprated engine, and new electronics and additional sensors
- F/A-14 ECR- (electronic combat/reconnaissance) suppression of enemy air defenses
- F/A-14B1 ECR-2- updated F/A-14 ECR with uprated engine, and new electronics and additional sensors
Specifications
- Crew: 2
- Length: 16.72 m (54 ft 10 in)
- Wingspan: 13.91 m at 25° wing sweep, 8.60 m at 67° wing sweep (45.6 ft / 28.2 ft)
- Height: 5.95 m (19.5 ft)
- Wing area: 26.6 m2 (286 ft2)
- Empty weight: 13,890 kg (31,620 lb)
- Max. takeoff weight: 28,000 kg (61,700 lb)
- Powerplant: 2 × afterburning turbofans
- Dry thrust: 46.76 kN (10,512 bf) each
- Thrust with afterburner: 82.18 kN (18,475 lbf) each
- Maximum speed: Mach 2.2 (2,400 km/h, 1,490 mph) at 9,000 m (30,000 ft) altitude
- Range: 1,390 km (870 mi) typical combat
- Ferry range: 3,890 km (2,417 mi) with four external drop tanks
- Service ceiling: 15,240 m (50,000 ft)
- Rate of climb: 76.7 m/s (15,100 ft/min)
- Thrust/weight: 0.55
- Guns: 1× 30 mm cannon internally mounted under left side of fuselage with 180 rounds
- Hardpoints: 4× light duty + 3× heavy duty under-fuselage and 4× swiveling under-wing pylon stations with a capacity of 9,000 kg (19,800 lb) of payload