Difference between revisions of "Triax F/A-25 Phoenix"
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| + | ==Overview== | ||
| + | |||
| + | ==Specifications== | ||
| + | '''Role:''' Advanced Multirole Fighter Aircraft<br/> | ||
| + | '''Crew:''' 1<br/> | ||
| + | '''Length:''' 58 ft. (17.68 m)<br/> | ||
| + | '''Wingspan:''' 41 ft. (12.5 m)<br/> | ||
| + | '''Wing Area:''' 475.48 ft² (44.17m²)<br/> | ||
| + | '''Height:''' 18.5 ft. (5.63 m)<br/> | ||
| + | '''Empty Weight:''' 28,000 lb. (12,700 kg)<br/> | ||
| + | '''Maximum Takeoff Weight:''' 64,000 lb.<br/> | ||
| + | '''Fuel Weight:''' 22,000 lb. (9,980 kg)<br/> | ||
| + | '''Power Plant:''' 2x AviaTech Dynamics FX1250-AD-25E fluid thrust vectoring low bypass turbofans<br/> | ||
| + | '''Maximum Thrust:''' 38,000 (169 kN) lbs dry, 60,000 (266.9 kN) with afterburners<br/> | ||
| + | '''Maximum Speed:''' Mach 2.6 with full afterburner, 2.2 super cruise<br/> | ||
| + | '''Initial Climb Rate:''' 45,000 ft/min (13,700 m/min)<br/> | ||
| + | '''Service Ceiling:''' 73,000 ft. (22.25 km)<br/> | ||
| + | '''Range:''' 1,800 miles (2,900 km) (full combat load) 4,100 miles (6,600 km) (ferry)<br/> | ||
| + | '''Airframe G-Limit:''' +13/7-<br/> | ||
| + | <br/><br/> | ||
| + | '''Weapons:'''<br/> | ||
| + | 2 × Main underside internal bays capable of carrying 1,200 lbs of stores<br/> | ||
| + | 2 × Secondary bays capable of holding one short ranged air-to-air missile each<br/> | ||
| + | 4 × Removable wing hard points<br/> | ||
| + | 2 × Wingtip hard points<br/> | ||
| + | 1 × 20mm internal rotary cannon<br/> | ||
| + | <br/><br/> | ||
| + | '''Systems:'''<br/> | ||
| + | 1 × Advanced Radar Detection System (ARADS) Integrated RADAR system incorporating a LPI AESA RADAR and passive detection systems.<br/> | ||
| + | 1 × Infrared Tracking System<br/> | ||
| + | 1 × Multipurpose Data-link<br/> | ||
| + | 1 × Tandem LA/LIDAR sensors<br/> | ||
| + | 1 × LADAR scrambling systems<br/> | ||
| + | 1 × IR Dazzlers<br/> | ||
| + | 1 × Multi-function physical countermeasures (chaff, flares) release system<br/> | ||
| + | 1 × Multi-function ECM/ECCM systems<br/> | ||
| + | 1 × Laser Inertial Navigation Systems<br/> | ||
| + | 1 × GPS receiver<br/> | ||
Revision as of 16:34, 17 December 2014
Overview
Specifications
Role: Advanced Multirole Fighter Aircraft
Crew: 1
Length: 58 ft. (17.68 m)
Wingspan: 41 ft. (12.5 m)
Wing Area: 475.48 ft² (44.17m²)
Height: 18.5 ft. (5.63 m)
Empty Weight: 28,000 lb. (12,700 kg)
Maximum Takeoff Weight: 64,000 lb.
Fuel Weight: 22,000 lb. (9,980 kg)
Power Plant: 2x AviaTech Dynamics FX1250-AD-25E fluid thrust vectoring low bypass turbofans
Maximum Thrust: 38,000 (169 kN) lbs dry, 60,000 (266.9 kN) with afterburners
Maximum Speed: Mach 2.6 with full afterburner, 2.2 super cruise
Initial Climb Rate: 45,000 ft/min (13,700 m/min)
Service Ceiling: 73,000 ft. (22.25 km)
Range: 1,800 miles (2,900 km) (full combat load) 4,100 miles (6,600 km) (ferry)
Airframe G-Limit: +13/7-
Weapons:
2 × Main underside internal bays capable of carrying 1,200 lbs of stores
2 × Secondary bays capable of holding one short ranged air-to-air missile each
4 × Removable wing hard points
2 × Wingtip hard points
1 × 20mm internal rotary cannon
Systems:
1 × Advanced Radar Detection System (ARADS) Integrated RADAR system incorporating a LPI AESA RADAR and passive detection systems.
1 × Infrared Tracking System
1 × Multipurpose Data-link
1 × Tandem LA/LIDAR sensors
1 × LADAR scrambling systems
1 × IR Dazzlers
1 × Multi-function physical countermeasures (chaff, flares) release system
1 × Multi-function ECM/ECCM systems
1 × Laser Inertial Navigation Systems
1 × GPS receiver
