Ausaine F6M Wasp: Difference between revisions
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==Operational History== | ==Operational History== | ||
==Variants== | ==Variants== |
Revision as of 16:53, 3 January 2025
Ausaine F6M Wasp | |
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F6M Wasp | |
Role | Multirole fighter |
National origin | Meridon |
Manufacturer | Ausaine Aerospace |
First flight | 14 August 1977 |
Introduction | 3 September 1986 |
Status | In active service |
Primary user | Meridonian Navy Meridonian Air Forces |
Produced | 1979-present |
Number built | 2,012 |
Unit cost |
86.2 million MD (F5M7)
|
The Ausaine F6M Wasp is a Meridonian carrier-capable, supersonic, twin engine, two seat, twin tail, multirole jet fighter built by Ausaine Aerospace. Designed to fit the needs of the Meridonian Navy to replace a variety of legacy aircraft conducting strike and air combat roles, particularly the A6M Raider and A7M Cutlass, it was designed to reduce operating costs by combining a large variety of roles into one aircraft. Adopted by the Meridonian Navy and later by the Meridonian Air Forces, the Wasp comprises the 'low' end of the 'high-low' mix of fighter aircraft.
The Wasp is designed and marketed as a multirole fighter aircraft, however it was designed with ground attack missions in mind- a role in which it complements the air warfare-oriented Gruening F5M Lynx in service. Wasp is capable of effectively conducting any missionset expected of a fighter aircraft, and is commonly used as a carrier-based refueler by the Navy. It pioneered a number of advancements, particularly in avionics, which became standard in the Meridonian aircraft. Designed for rugged operations from both carrier and land short fields and ease of maintenance, its well-balanced aerodynamic characteristics and versatility have also made it a popular escort aircraft, forming the mainstay of a number of foreign militaries. Meridonian variants have been upgraded to the F6M2 variant, which includes advanced avionics and the introduction of an infrared search and track system.
Development
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Design
Operational History
Variants
- F6M
- Initial operational variant, first supplied to the Meridonian Navy in 1974. As initially supplied, it was almost purely an interceptor and air superiority aircraft, with marginal ground strike capability added through unguided bombs and rockets only. It was powered by Altern MG-410 afterburning turbofans, which proved unreliable and prone to compressor stalls especially at high AOAs. All F5M models were upgraded to F5M2 standard by 1983.
- F6M2
- Upgraded variant of the initial F5M2 variant addressing numerous concerns by the Navy and adding operational requirements for use by the Air Force. Wing vanes mounted in the glove box were permanently removed, and the addition of a second CRT display for navigation was included. Integration with civilian navigational sources including VOR and ILS were integrated for use, including a HUD approach mode. Automatic Carrier Landing System (ACLS) capability was added to this model. A total of 103 F5Ms were upgraded, and an additional 242 were produced to F5M2 standard.
- E6M2 Backwave
- Upgrade program conducted in the mid-late 1980s, its primary improvement was replacing the unreliable Altern MG-410 engines with Hollon FT80s, which themselves were a product of the failed Air Supremacy Initiative. Performance increases were substantial, allowing even a fully-loaded fighter to take off without the use of afterburner, a feat unmatched by any other model of naval fighter before or since. Integration was added for the TANDEM NAVLFIR system, including the employment of laser-guided bombs.
Operators
Current Operators
- Meridon- 1,600 have been built for the Meridon Defense Forces. All variants have been upgraded to F6M2 standard.
Specifications (F6M2)
General Characteristics
- Crew: 2
- Length: 50 ft 10 in (15.5m)
- Wingspan: 39ft 6.6 in (12.05m)
- Height: 13 ft 10 in (4.2 m)
- Wing Area: 494 sq ft (45.9 m2)
- Empty Weight: 26,700 lb (11,203 kg)
- Max Takeoff Weight: 62,400lb (28,304 kg)
- Powerplant: 2 × Hollon FT94E afterburning turbofans, producing 13,500lbf (60 kN) each dry, 20,200lbf (90 kN) in afterburner
- Fuel Capacity: 15,500lb internal, up to 5x optional 480gal (3,260lb/1,478kg each) external tanks
Performance
- Maximum Speed: Mach 1.34 (1465 km/h, 909 mph) at altitude
- Service Ceiling: 50,000 ft (15,240 m) +
- Rate of Climb: 45,304 ft/min plus (230 m/s)+
- Wing Loading: 126.2 lb/sq ft (617.6 kg/m2)
- Thrust/Weight: 0.647 at MGTOW
Armament
- Guns: 1 × Mark 40 25mm cannon with 520 rounds
- Payload: 13 hardpoints total: 4 per wing, 5 fuselage stations with total capacity of 20,000lbs of payload
Avionics
- TA-940C active electronically scanned array radar
- AE-161B radar warning receiver
- AI-50B infrared search/track
- AI-20B missile approach warning system
- AE-202C Electronic Warfare/ Defensive Electronic Countermeasures System