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| ASh-82 (65k) and ASh-82FN (58k) engines, courtesy of Sergey Andreev; | |||
| Cylinder diameter | 155.5mm |
| Cylinder motion | 155...156mm |
| Engine volume | 41.2l |
| Compression ratio | 6.9 (+0.15 -0.1) |
| Operation regime | Power hp | Rate rpm | Fuel consumption g/hp/h |
|---|---|---|---|
| Ground normal | 1150 | 2400 | 285...315 |
| Ground maximal | 1430 | 2400 | 315...340 |
| Takeoff | 1700 | 2600 | 325...360 |
| Cruise at 1550m | 1530 | 2400 | ? |
| Cruise at 4550m | 1330 | 2400 | ? |
| ASh-82, M-82 |
1940? | 14cyl 2-raw a.c. | 1330hp |
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| ASh-82A M-82A |
1942? | a.c. | 1330/1600hp |
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| ASh-82F M-82F |
1941 | a.c. | 1400/1675hp |
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| M-82FN M-82FN |
1943? | 14cyl. a.c. fuel injection | 1460hp/1850hp | |||||||||||
| ASh-82-? | 1947? | a.c. | 2100hp |
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| ASh-82T | 1953? | a.c. | 1900hp |
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| ASh-82V | 1952? | a.c. | 1200kW, 1700hp |
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| Created long ago,
Modified October 26, 1998 by Sergey Andreev and Alexandre Savine |
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