M-82, ASh-82, A.D.Shvetsov
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| ASh-82 (65k) and ASh-82FN (58k) engines, courtesy of ; |
One of the most successful Soviet piston engines of the World War II era.
Some data on the ASh-82V engine:
| 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 |
? |
Regular fuel (Gasoline) B-95/130 (GOST 1012-54), Oil MK-22 or MS-20 (GOST 1013-49)
References:
[1] Aviation engine Ash-82V, technical description. OBORONGIZ, 1963, 178 pp.
ASh-82, M-82
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1940?
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14cyl 2-raw a.c. |
1330hp |
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ASh-82A
M-82A |
1942?
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a.c. |
1330/1600hp |
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ASh-82F
M-82F |
1941
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a.c. |
1400/1675hp |
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M-82FN
M-82FN |
1943?
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14cyl. a.c. fuel injection |
1460hp/1850hp |
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| ASh-82-? |
1947?
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a.c. |
2100hp |
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| ASh-82T |
1953?
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a.c. |
1900hp |
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| ASh-82V |
1952?
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a.c. |
1200kW, 1700hp |
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