Mikoyan-Gurevich MiG-9
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Re: Mikoyan-Gurevich MiG-9
Service
The I-300 reached a speed of 910 km/h (565 mph) during initial tests, and after further refinement, it entered service with the [Vous devez être inscrit et connecté pour voir ce lien] as the MiG-9 during the winter of 1946-47.
The jet had many performance- and steering-related problems, however it was put into service mainly because of political considerations.
These led directly to the death of Alexei N. Grinchik on 11 July 1946 when he crashed a prototype I-300 while flying demonstration flights for the VVS leadership and government officials.
The I-300 reached a speed of 910 km/h (565 mph) during initial tests, and after further refinement, it entered service with the [Vous devez être inscrit et connecté pour voir ce lien] as the MiG-9 during the winter of 1946-47.
The jet had many performance- and steering-related problems, however it was put into service mainly because of political considerations.
These led directly to the death of Alexei N. Grinchik on 11 July 1946 when he crashed a prototype I-300 while flying demonstration flights for the VVS leadership and government officials.
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Re: Mikoyan-Gurevich MiG-9
The final production MiG-9 was allocated the [Vous devez être inscrit et connecté pour voir ce lien] of "Fargo" and the Soviet designation I-301.
Later designs of the MiG-9 attempted to resolve many of the issues encountered in the I-300, including the fit of a rectangular fin to the 37 millimeter cannon barrel, giving the configuration the nickname "The Butterfly", however none of them worked very well.
Later designs of the MiG-9 attempted to resolve many of the issues encountered in the I-300, including the fit of a rectangular fin to the 37 millimeter cannon barrel, giving the configuration the nickname "The Butterfly", however none of them worked very well.
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Re: Mikoyan-Gurevich MiG-9
In the end, the entire nose was redesigned with the cannon barrel muzzles moved behind the engine intake and with the cockpit moved forward.
The result was the single "MiG-9M", which also featured an ejection seat and RD-21 engines, the RD-21 being an afterburning variant of the RD-20 / BMW-003.
The MiG-9 was deployed largely in the ground-attack role and 610 aircraft were built in different versions by the time production ended in 1948.
The result was the single "MiG-9M", which also featured an ejection seat and RD-21 engines, the RD-21 being an afterburning variant of the RD-20 / BMW-003.
The MiG-9 was deployed largely in the ground-attack role and 610 aircraft were built in different versions by the time production ended in 1948.
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Re: Mikoyan-Gurevich MiG-9
MiG-9 (F) : "aircraft F" - the only serial variant, RD-20 engines
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Re: Mikoyan-Gurevich MiG-9
MiG-9 (FP) : "aircraft FP", I-302 - prototype with modified weapons layout
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MiG-9 (FL) : "aircraft FL", I-305 - variant with Lyulka TR-1A engines, not completed
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Re: Mikoyan-Gurevich MiG-9
MiG-9 (FF) : "aircraft FF", I-307 - prototypes with afterburned RD-20F or RD-21 engines
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MiG-9M (FR) : "aircraft FR", I-308 - modified prototypes with RD-21 engines
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Re: Mikoyan-Gurevich MiG-9
MIG-9UTI : Two-seat training aircraft. Around 80 built. Also known as the I-301T.
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Re: Mikoyan-Gurevich MiG-9
Specifications (MiG-9)
Data from The Great Book of Fighters
General characteristics
Data from The Great Book of Fighters
General characteristics
- Crew: One
- Length: 9.83 m (32 ft 3 in)
- [Vous devez être inscrit et connecté pour voir ce lien]: 10 m (32 ft 10 in)
- Height: 3.22 m (10 ft 7 in)
- Wing area: 18.20 m² (195.9 ft²)
- [Vous devez être inscrit et connecté pour voir ce lien]: 3,420 kg (7,540 lb)
- Loaded weight: 4,965 kg (10,945 lb)
- [Vous devez être inscrit et connecté pour voir ce lien]: 5,500 kg (12,125 lb)
- Powerplant: 2× [Vous devez être inscrit et connecté pour voir ce lien] [Vous devez être inscrit et connecté pour voir ce lien], 7.8 kN (1754 lbf)[Vous devez être inscrit et connecté pour voir ce lien] each
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