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Shvetsov ASh-21
Soviet radial piston aircraft engine
Soviet radial piston aircraft engine
| Field | Value |
|---|---|
| name | ASh-21 |
| image | Petőfi Csarnok, Repüléstörténeti kiállítás, Švecov Aš-21.JPG |
| engine_type | Radial engine |
| manufacturer | Shvetsov OKB-19 in Perm' |
| first_run | 1945 |
| number_built | 7,636 |
| developed_from | Shvetsov ASh-82 |
The Shvetsov ASh-21 (Russian: Швецов АШ-21) is a seven-cylinder single-row air-cooled radial aero engine.
Design and development
The ASh-21 is basically a single-row version of the Shvetsov ASh-82. The ASh-21 also incorporates a number of parts from the ASh-62 radial engine. Design began in 1945, and by 1947 testing had finished and production had begun. Between 1947 and 1955 7,636 ASh-21 engines had been built in the USSR and beginning in 1952 it was produced in Czechoslovakia as the M-21.
Applications
- Beriev Be-8
- Beriev Be-30 (prototype)
- Yakovlev Yak-11
- Yakovlev Yak-16
Specifications (Shvetsov ASh-21)

| and start a new, fully-formatted line with -- ||power=
- 520 kW (700 hp) at 2,300 rpm takeoff power
- 459 kW (615 hp) at 1,700 m (5,580 ft) |power/weight=1.07 kW/kg (0.65 hp/lb)
References
This article was imported from Wikipedia and is available under the Creative Commons Attribution-ShareAlike 4.0 License. Content has been adapted to SurfDoc format. Original contributors can be found on the article history page.
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