Myasishchev M-200
| Myasishchev M-200 | |
|---|---|
| Type: | Jet trainer |
| Design country: | |
| Manufacturer: | |
| Number of pieces: |
2 prototypes |
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The Mjasishchev M-200 ( Russian Мясищев М-200 ) was the project of a Russian jet trainer.
history
For the successor to the now outdated Aero L-39 trainer in the Soviet Air Force , the so-called UTS specification was issued to various Soviet design offices in 1991.
The M-200 (UTS) was then built in the Myasishchev design office. Like its predecessor, the L-39, this was equipped with a tandem cockpit. The two jet engines were housed in short nacelles, which were arranged at the wing root below the wing. The landing gear consisted of a nose wheel with single tires and two main landing gears, also with single tires.
The designs Jakowlew Jak-130 , Mikojan-Gurevich MiG-AT , Myasishchev M-200 and Sukhoi S-54 took part in the competition, the decision was made in May 1992 in favor of the Jak-130 and initially also the MiG-AT, all of them other projects have been discontinued. After building two prototypes, the development of the MiG-AT was also ended.
Technical specifications
| Parameter | Data |
|---|---|
| Construction year | 1994 (project) |
| Manufacturer | Myasishchev |
| crew | 2 |
| length | 10.37 m |
| span | 9.40 m |
| height | 4.20 m |
| Gauge | 2.70 m |
| wheelbase | 4.30 m |
| Empty mass | 3805 kg |
| Fuel load | 1380 kg |
| Cruising speed | 700 km / h |
| Top speed | ? km / h |
| Service ceiling | 13,100 m |
| Max. Range | 1400 km |
| Engines | 2 R-35 |
literature
- Wilfried Copenhagen , Jochen K. Beeck: The large aircraft type book . Motorbuch, Stuttgart 2005, ISBN 978-3-613-02522-6 , p. 498 .