Difference between revisions of "Triax F/A-25 Phoenix"
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[[Category:Californian Empire]] | [[Category:Californian Empire]] | ||
+ | {| class="toccolours" style="float: right; width: 350px;" border="0" cellpadding="2" cellspacing="0" | ||
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+ | | colspan="2" style="background: #CC0000; color: #FFFFFF;" align="center" | <big>'''F/A-25E/F Phoenix AFX'''</big> | ||
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+ | | align="center" colspan="2" | [[File: -- g|320px|center]] | ||
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+ | | align="center" colspan="2" | <small>TAEC F/A-25E Phoenix</small> | ||
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+ | | colspan="2" | <hr> | ||
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+ | | style="font-size: 90%;" | '''Role''' || style="font-size: 90%;" | Advanced [[wikipedia:Multirole_combat_aircraft|Multirole Fighter]] | ||
+ | |- | ||
+ | | style="font-size: 90%;" | '''National Origin''' || style="font-size: 90%;" | [[Nation/Californian_Empire|Californian Empire]] | ||
+ | |- | ||
+ | | style="font-size: 90%;" | '''Manufacturer''' || style="font-size: 90%;" | Triax Aeronautics Engineering Corporation | ||
+ | |- | ||
+ | | style="font-size: 90%;" | '''First Flight''' || style="font-size: 90%;" | 7 September 2xxx | ||
+ | |- | ||
+ | | style="font-size: 90%;" | '''Introduction''' || style="font-size: 90%;" | 15 December 2xxx | ||
+ | |- | ||
+ | | style="font-size: 90%;" | '''Status''' || style="font-size: 90%;" | In service | ||
+ | |- | ||
+ | | style="font-size: 90%;" | '''Primary Users''' || style="font-size: 90%;" | Californian Empire | ||
+ | |- | ||
+ | | style="font-size: 90%;" | '''Produced''' || style="font-size: 90%;" | 2xxx-2xxx | ||
+ | |- | ||
+ | | style="font-size: 90%;" | '''Number Built''' || style="font-size: 90%;" | 1,108 (8 test and 1,100 operation aircraft) | ||
+ | |- | ||
+ | | style="font-size: 90%;" | '''Program Cost''' || style="font-size: 90%;" | Đ31.1 billion CES ($66.7 billion USD) | ||
+ | |- | ||
+ | | style="font-size: 90%;" | '''Unit Cost''' || style="font-size: 90%;" | Đ69.77 million CES ($150 million USD) | ||
+ | |- | ||
+ | | style="font-size: 90%;" | '''Developed From''' || style="font-size: 90%;" | TAEC F/A-24D Wraith, TAEC YF-25 | ||
+ | |- | ||
+ | | style="font-size: 90%;" | '''Developed Into''' || style="font-size: 90%;" | TAEC F/A-25A-F | ||
+ | |- | ||
+ | | style="font-size: 90%;" | '''Variants''' || style="font-size: 90%;" | TAEC F/A-25A Viper, TAEC F/A-25B/C Strike Viper, F/A-25D Fighting Phoenix, F/A-25E/F Strike Phoenix | ||
+ | |- | ||
+ | |} | ||
==Overview== | ==Overview== |
Revision as of 16:56, 17 December 2014
F/A-25E/F Phoenix AFX | |
TAEC F/A-25E Phoenix | |
| |
Role | Advanced Multirole Fighter |
National Origin | Californian Empire |
Manufacturer | Triax Aeronautics Engineering Corporation |
First Flight | 7 September 2xxx |
Introduction | 15 December 2xxx |
Status | In service |
Primary Users | Californian Empire |
Produced | 2xxx-2xxx |
Number Built | 1,108 (8 test and 1,100 operation aircraft) |
Program Cost | Đ31.1 billion CES ($66.7 billion USD) |
Unit Cost | Đ69.77 million CES ($150 million USD) |
Developed From | TAEC F/A-24D Wraith, TAEC YF-25 |
Developed Into | TAEC F/A-25A-F |
Variants | TAEC F/A-25A Viper, TAEC F/A-25B/C Strike Viper, F/A-25D Fighting Phoenix, F/A-25E/F Strike Phoenix |
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