Two-seat training version of fighter MiG-21.
First fly of MiG-21U (two-place version of MiG-21F-13) take place in 30th of October 1960. Later versions was MiG-21US and MiG-21UM. A total of 1133 MiG-21UM were built.
Specifications of MiG-21UM: |
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| wing span: | 7,15 m |
| length: | 12,18 m |
| height: | 4,80 m |
| wing area: | 22,95 m2 |
| weight: | |
| - empty aircraft | 5610 kg |
| - normal take-off | 8000 kg |
| Internal fuel | 2030 kg |
| engine: | R-11F2S-300 |
| maximal thrust: | 64,70 kN |
| maximal speed: | |
| - at ground level | 1150 km/h |
| - in altitude 12000 m | 2230 km/h |
| range: | 1760 km |
| service ceiling: | 17300 m |
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[770x343px 58 kB] |
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© Kamil Pankuch 2004-2007
airmuseum.kosice at gmail.com
