Difference between revisions of "Triax AB-121 Nightshade"
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+ | {| class="toccolours" style="float: right; width: 350px;" border="0" cellpadding="2" cellspacing="0" | ||
+ | |- | ||
+ | | colspan="2" style="background: #CC0000; color: #FFFFFF;" align="center" | <big>'''F/A-25E/F Strike Phoenix AFX'''</big> | ||
+ | |- | ||
+ | | align="center" colspan="2" | [[File:1024px-FA-25E.jpg|320px|center]] | ||
+ | |- | ||
+ | | align="center" colspan="2" | <small>TAEC F/A-25E Phoenix</small> | ||
+ | |- | ||
+ | | colspan="2" | <hr> | ||
+ | |- | ||
+ | | style="font-size: 90%;" | '''Role''' || style="font-size: 90%;" | Advanced [[wikipedia:Stealth_aircraft|Stealth]] [[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/A-25B/C, F/A-25D, F/A-25E/F | ||
+ | |- | ||
+ | | style="font-size: 90%;" | '''Variants''' || style="font-size: 90%;" | TAEC F/A-25A Viper, F/A-25B/C Strike Viper, F/A-25D Fighting Phoenix, F/A-25E/F Strike Phoenix | ||
+ | |- | ||
+ | |} | ||
+ | |||
+ | ==Overview== | ||
+ | |||
+ | ==Specifications== | ||
+ | ===General Characteristics=== | ||
+ | * '''Role:''' Advanced [[wikipedia:Stealth_aircraft|Stealth]] [[wikipedia:Multirole_combat_aircraft|Multirole Fighter]] | ||
+ | * '''Crew:''' 1 | ||
+ | * '''Length:''' 58 ft. (17.68 m) | ||
+ | * '''[[wikipedia:Wingspan|Wingspan]]:''' 41 ft. (12.5 m) | ||
+ | * '''Wing area:''' 804.72 ft² (74.76 m²) | ||
+ | * '''Height:''' 18.5 ft. (5.63 m) | ||
+ | * '''[[wikipedia:Manufacturer%27s_Weight_Empty|Empty weight]]:''' 41,500 lb. (18,830 kg) | ||
+ | * '''Loaded weight:''' 63,140 lb. (28,640 kg) | ||
+ | * '''[[wikipedia:Maximum_takeoff_weight|Max. takeoff weight]]:''' 81,800 lb. (37,100 kg) | ||
+ | * '''[[wikipedia:Aircraft_engine|Powerplant]]:''' 2x AviaTech Dynamics FX1250-AD-25E fluid thrust vectoring low bypass [[wikipedia:Turbofan|turbofans]] | ||
+ | **'''Dry Thrust:''' 19,000 (84.5 kN) lbs each | ||
+ | ** '''Thrust with [[wikipedia:Afterburner|afterburner]]:''' 30,000+ lbs (133.45 kN) each | ||
+ | * '''Fuel Capacity:''' 18,000 lb (8,200 kg) internally, or 26,000 lb (12,000 kg) with two external fuel tanks<br/> | ||
+ | |||
+ | ===Performance=== | ||
+ | * '''[[wikipedia:V_speeds#Regulatory_V-speeds|Maximum Speed]]:''' | ||
+ | ** '''At altitude:''' [[wikipedia:Mach_number|Mach]] 2.6 with full afterburner | ||
+ | ** '''[[wikipedia:Supercruise|Supercruise]]:''' Mach 2.2 | ||
+ | * '''[[wikipedia:Range_(aircraft)|Range]]:''' 1,800 miles (2,900 km) (full combat load) | ||
+ | * '''[[wikipedia:Combat_radius|Combat radius]]:''' 410 nmi (with 100 nmi in supercruise) (470 mi, 760 km) | ||
+ | * '''[[wikipedia:Range_(aircraft)|Ferry range]]:''' 4,100 miles (6,600 km) | ||
+ | * '''[[wikipedia:Ceiling_(aircraft)|Service Ceiling]]:''' 73,000 ft. (22.25 km) | ||
+ | * '''[[wikipedia:Wing_loading|Wing loading]]:''' 78.4 lb/ft² (383 kg/m²) | ||
+ | * '''[[wikipedia:Thrust-to-weight_ratio|Thrust/weight]]:''' 0.95 | ||
+ | * '''Maximum design [[wikipedia:Standard_gravity|''g'']]-load:''' -7/+13 ''g'' | ||
+ | * '''Initial Climb Rate:''' 45,000 ft/min (13,700 m/min) | ||
+ | |||
+ | ===Armament=== | ||
+ | * '''Guns:''' 1 × [[wikipedia:20_mm_caliber|20mm]] internal rotary cannon | ||
+ | * '''Air to air loadout:''' | ||
+ | ** 6 × [[wikipedia:AIM-120_AMRAAM|AIM-120 AMRAMM]] carried in Secondary bays | ||
+ | ** 2 × [[wikipedia:AIM-9_Sidewinder|AIM-9 Sidewinder]] carried in internal bays | ||
+ | * '''Air to ground loadout:''' | ||
+ | ** 2 × 1,000 lb (450 kg) [[wikipedia:Joint_Direct_Attack_Munition|JDAM]] or 8× 250 lb (110 kg) [[wikipedia:GBU-39_Small_Diameter_Bomb|GBU-39 Small Diameter Bombs]] | ||
+ | ** 2 × AIM-120 AMRAAM | ||
+ | ** 2 × AIM-9 Sidewinder | ||
+ | * '''[[wikipedia:Hardpoint|Hardpoints]]''' 4× under-wing pylon stations can be fitted to carry 600 U.S. [[wikipedia:Gallon|gallon]] [wikipedia:Drop_tank|drop tanks]] or weapons, each with a capacity of 5,000 lb (2,270 kg). | ||
+ | |||
+ | ===Avionics=== | ||
+ | * Advanced Radar Detection System (ARADS) Integrated [[wikipedia:Radar|RADAR]] system incorporating a [[wikipedia:Low_probability_of_intercept_radar|LPI]] [[wikipedia:Active_electronically_scanned_array|AESA]] RADAR and passive detection systems. | ||
+ | * AN/AAR-73 [[wikipedia:Missile_approach_warning|Missile Launch Detection]] (MLD) | ||
+ | * [[wikipedia:Radar_warning_receiver|Radar warning receiver]] (RWR) 450 nmi (833.40 km) or more detection range | ||
+ | * [[wikipedia:Infrared|Infrared]] Tracking System | ||
+ | * Multipurpose [[wikipedia:Tactical_Data_Link|Tactical Datalink]] | ||
+ | * Tandem [[wikipedia:LIDAR|LADAR/LIDAR]] sensors | ||
+ | * [[wikipedia:LIDAR|LADAR]] scrambling systems | ||
+ | * [[wikipedia:Infrared|IR]] [[wikipedia:Dazzler_(optical_device)|Dazzlers]] | ||
+ | * Multi-function [[wikipedia:Countermeasure|physical countermeasures]] (chaff, flares) release system | ||
+ | * Multi-function [[wikipedia:Electronic_countermeasure|ECM]]/[[wikipedia:Electronic_counter-countermeasures|ECCM]] systems | ||
+ | * [[wikipedia:Laser|Laser]] [[wikipedia:Inertial_navigation_system|Inertial Navigation Systems]] | ||
+ | * [[wikipedia:GPS_Aircraft_Tracking|GPS receiver]] | ||
+ | * [[wikipedia:Leading-edge_slats|Slat]] L-band arrays for [[wikipedia:Identification_friend_or_foe|IFF]] | ||
+ | * SDX-105 Multifunctional Integrated [[wikipedia:Digital_electronics|Digital Electronic]] System (MIDES) | ||
[[Category:Californian Empire]] | [[Category:Californian Empire]] |
Revision as of 20:56, 17 December 2014
This page is a work in progress by its author(s) and should not be considered final. |
F/A-25E/F Strike Phoenix AFX | |
TAEC F/A-25E Phoenix | |
| |
Role | Advanced Stealth 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/A-25B/C, F/A-25D, F/A-25E/F |
Variants | TAEC F/A-25A Viper, F/A-25B/C Strike Viper, F/A-25D Fighting Phoenix, F/A-25E/F Strike Phoenix |
Contents
Overview
Specifications
General Characteristics
- Role: Advanced Stealth Multirole Fighter
- Crew: 1
- Length: 58 ft. (17.68 m)
- Wingspan: 41 ft. (12.5 m)
- Wing area: 804.72 ft² (74.76 m²)
- Height: 18.5 ft. (5.63 m)
- Empty weight: 41,500 lb. (18,830 kg)
- Loaded weight: 63,140 lb. (28,640 kg)
- Max. takeoff weight: 81,800 lb. (37,100 kg)
- Powerplant: 2x AviaTech Dynamics FX1250-AD-25E fluid thrust vectoring low bypass turbofans
- Dry Thrust: 19,000 (84.5 kN) lbs each
- Thrust with afterburner: 30,000+ lbs (133.45 kN) each
- Fuel Capacity: 18,000 lb (8,200 kg) internally, or 26,000 lb (12,000 kg) with two external fuel tanks
Performance
- Maximum Speed:
- At altitude: Mach 2.6 with full afterburner
- Supercruise: Mach 2.2
- Range: 1,800 miles (2,900 km) (full combat load)
- Combat radius: 410 nmi (with 100 nmi in supercruise) (470 mi, 760 km)
- Ferry range: 4,100 miles (6,600 km)
- Service Ceiling: 73,000 ft. (22.25 km)
- Wing loading: 78.4 lb/ft² (383 kg/m²)
- Thrust/weight: 0.95
- Maximum design g-load: -7/+13 g
- Initial Climb Rate: 45,000 ft/min (13,700 m/min)
Armament
- Guns: 1 × 20mm internal rotary cannon
- Air to air loadout:
- 6 × AIM-120 AMRAMM carried in Secondary bays
- 2 × AIM-9 Sidewinder carried in internal bays
- Air to ground loadout:
- 2 × 1,000 lb (450 kg) JDAM or 8× 250 lb (110 kg) GBU-39 Small Diameter Bombs
- 2 × AIM-120 AMRAAM
- 2 × AIM-9 Sidewinder
- Hardpoints 4× under-wing pylon stations can be fitted to carry 600 U.S. gallon [wikipedia:Drop_tank|drop tanks]] or weapons, each with a capacity of 5,000 lb (2,270 kg).
Avionics
- Advanced Radar Detection System (ARADS) Integrated RADAR system incorporating a LPI AESA RADAR and passive detection systems.
- AN/AAR-73 Missile Launch Detection (MLD)
- Radar warning receiver (RWR) 450 nmi (833.40 km) or more detection range
- Infrared Tracking System
- Multipurpose Tactical Datalink
- Tandem LADAR/LIDAR sensors
- LADAR scrambling systems
- IR Dazzlers
- Multi-function physical countermeasures (chaff, flares) release system
- Multi-function ECM/ECCM systems
- Laser Inertial Navigation Systems
- GPS receiver
- Slat L-band arrays for IFF
- SDX-105 Multifunctional Integrated Digital Electronic System (MIDES)