Kyrkeyev Ky-44 Strigon: Difference between revisions
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Ky-44 Strigon | |
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File:Ky-44 iiwiki.png | |
General information | |
Type | Air superiority fighter |
Manufacturer | Kyrkeyev Design Bureau |
Status | In development |
History | |
Manufactured | 2015-present |
Introduction date | 1 January 2006 |
The Kyrkeyev Ky-44 Strigon (Stasnovan: TBA) is Stasnovan twin-engine, canard delta wing air superiority aircraft, curretnly in development. The Ky-44 was designed and built mostly as a testbed for the new VNRS-97 weapons system. It's uknown wether or not this aircraft will enter full service with the Stasnovan VVS. It has been developed and designed by the Kyrkeyev Design Bureau.
Origins
Further Development
Design
Operational history
Variants
Operators
Specifications (VeK-29S)
Specifications (VeK-29M)
General characteristics
- Crew: 1: pilot
- Length: 20.40 m ()
- Wingspan: 12.40 m ()
- Height: 3.99 m ()
- Empty weight: TBA kg ()
- Loaded weight: TBA kg ()
- Max. takeoff weight: TBA kg ()
- Powerplant: 2 × Krasna ZK/Y-64 (assumed) afterburning turbofans
Performance
- Maximum speed: Mach 2.4 (assumed)
- Combat radius: TBA km ()
- Service ceiling: TBA m ()
- Rate of climb: TBA m/s ()
- Maximum design g-load: +12 g
Armament
- Guns: Provision for 1× 30 mm GSh-301 cannon (assumed)
- Hardpoints: Total of TBA and provisions to carry combinations of:
- Other: TBA
- Missiles:
- Air-to-air missiles:
- Air-to-surface missiles
- Bombs:
Avionics
TBA