M-82, ASh-82, A.D.Shvetsov
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
|
1940? |
14cyl 2-raw a.c. |
1330hp |
|
ASh-82A M-82A |
1942? |
a.c. |
1330/1600hp |
|
ASh-82F M-82F |
1941 |
a.c. |
1400/1675hp |
|
M-82FN M-82FN |
1943? |
14cyl. a.c. fuel injection |
1460hp/1850hp |
|
| ASh-82-? |
1947? |
a.c. |
2100hp |
|
| ASh-82T |
1953? |
a.c. |
1900hp |
|
| ASh-82V |
1952? |
a.c. |
1200kW, 1700hp |
|