Difference between revisions of "F/A-210"
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===F/A-210A=== | ===F/A-210A=== | ||
Revision as of 16:18, 1 October 2006
The F/A-210 is a new aircraft developed by Military Armament Company, Inc. for use with Asgarnian Collective Armed Forces air forces and The Asgarnian Air Force/Asgarnian Air Defense Force. It made its first flight on September 10, 2006.
Contents
Specifications
- Primary Functions
- Land-Based Strike Fighter
- Land-Based Attack Fighter
- Land-Based Light Bomber
- Builder
- Power Plant
- 2 David & David TF-787L Turbofan Jet Engines
- Thrust
- 39,354 Lbs per engine
- Length
- 63 Feet, 7 Inches
- Height
- 19 Feet, 11 Inches
- Wingspan
- 50 Feet, 6 Inches
- Canard Span
- 16 Feet, 10 Inches
- Weight
- 35,069 Empty
- 45,500 Max Takeoff
- Ceiling
- 36,210 Feet
- Speed
- 1,821 Miles Per Hour at Max Altitude
- 1,210 Miles Per Hour at Super Cruise
- Armament
- 2 30mm Multibarrelled Cannons (Military Armament Company, Inc.)
- 1 37mm Super Power Light Cannon (Hispano-Suiza)
- 2 AAM-74/C Long-Range Radar Guided Missiles (Military Armament Company, Inc.)
- Up to 5,000 Lbs In ECM, Cameras, Bombs, External Fuel Stores
- 4 AGM-29 Super Quell Air-to-Ground Missiles (Military Armament Company, Inc.)
- 6 BGM-13 Dunker GPS Guided Bombs (Military Armament Company, Inc.)
- Service Date
- October 1, 2006
- Range
- Classified
- Crew
- 2
- Pilot (Officer)
- Weapons Officer (Officer)
- 2
- Nation of Origin
Other Data
- Countermeasures
- Flares (32)
- Chaff Dispensers (20 Lbs)
- Jamming Pods
- Radar
- AA/PEQ-204 Long Range Multi-Target Tactical Radar
- Ejection Seats
- 2
- Selected Electronic Equipment
- AA/PEQ-37 Radar Lock Detector
- AA/PEQ-84 Laser Guidance Module
- HUD-EX/47 Upgraded Next-Generation Heads-Up Display
Variants
| Military Armament Company, Inc. F/A-210 Variants | ||||||||
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F/A-210A
- Air Superority Fighter
F/A-210B
- Light Bomber
F/A-210C
- Close Air Support
F/A-210D
- Ground Attack
F/A-210E
- Tactical Reconnaissance/Electronic Warfare
