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- Shvetsov_ASh-82 abstract "The Shvetsov ASh-82 (M-82) is a 14-cylinder, two-row, air-cooled radial aircraft engine developed from the Shvetsov M-62. The M-62 was the result of development of the M-25, which was a licensed version of the Wright R-1820 Cyclone.".
- Shvetsov_ASh-82 thumbnail Aircraft_engine_Shvetsov_ASh-82T.JPG?width=300.
- Shvetsov_ASh-82 wikiPageID "1899060".
- Shvetsov_ASh-82 wikiPageRevisionID "580639475".
- Shvetsov_ASh-82 bore "155.5".
- Shvetsov_ASh-82 compression "7.05".
- Shvetsov_ASh-82 coolingsystem "Air-cooled. Minimum permissible cylinders temp for operation: 120°C. Maximum permissible cylinders temp: 250°C. Maximum permissible at cruise: 225°C. Normal cylinders temp at cruise: 160 to 180°C".
- Shvetsov_ASh-82 developedFrom Shvetsov_ASh-62.
- Shvetsov_ASh-82 developedInto Shvetsov_ASh-21.
- Shvetsov_ASh-82 diameter "1.26 m".
- Shvetsov_ASh-82 displacement "41.2107".
- Shvetsov_ASh-82 fuelsystem "Carburettors , direct fuel injection with automatic mixture control. Petrol pump: BNK-10KT.".
- Shvetsov_ASh-82 fueltype "90".
- Shvetsov_ASh-82 generators "GDS-6000A 150 Amp".
- Shvetsov_ASh-82 hasPhotoCollection Shvetsov_ASh-82.
- Shvetsov_ASh-82 length "2.01 m".
- Shvetsov_ASh-82 lists "*List of aircraft engines".
- Shvetsov_ASh-82 magnetos "Two MB14T-2M".
- Shvetsov_ASh-82 manufacturer "Shvetsov & Evich, OKB-19 in Perm'".
- Shvetsov_ASh-82 numberBuilt "70000".
- Shvetsov_ASh-82 oilsystem "Two pumps: geared rotation pump MSH-6SV and swarm pump PMN-T . Normal oil temp: 40 to 90°C. Limit temp: 115°C. Minimum oil pressure at low gas: 3 kg/cm2 . Minimum oil pressure at cruise: 4.5 kg/cm2 , 5.5 kg/cm2".
- Shvetsov_ASh-82 power "*M-82-111 with carburettors: *1,570 hp at 2,400 RPM for take-off , boost rated at 1.55 Atm *1,540 hp at 2,400 RPM at 6,656 ft *1,330 hp at 2,400 RPM at 17,716 ft , boost rated at 1.29 Atm * 820 hp at 2,400 RPM at 27,887 ft *M-82FN with direct fuel injection: *1,650 hp at 2,400 RPM for take-off , boost rated at 1.55 Atm *1,430 hp at 2,400 RPM at 16,404 ft *800 hp at 2,400 RPM at 32,808 ft *M-82FNU: *1,850 hp at 2,500 RPM for take-off , boost rated at 1.60 Atm *1,650 hp at 2,400 RPM at 5,413 ft , boost rated at 1.36 Atm *1,450 hp at 2,400 RPM at 15,156 ft , boost rated at 1.36 Atm *810 hp at 2,400 RPM at 34,448 ft *M-82T with two speed supercharger: *1,900 hp at 2,600 RPM for take-off, boost rated at 1.64 Atm *1,630 hp at 2,400 RPM at 6,561 ft , boost rated at 1.34 Atm *1,530 hp at 2,400 RPM at 13,123 ft , boost rated at 1.34 Atm *721 hp at 2,400 RPM at 31,167 ft".
- Shvetsov_ASh-82 weight "1.46".
- Shvetsov_ASh-82 reductionGear "11".
- Shvetsov_ASh-82 similarEngines "*BMW 801 *Bristol Hercules *Fiat A.74 *Gnome-Rhône 14N *Mitsubishi Kinsei *Nakajima Sakae *Pratt & Whitney R-1830 *Wright R-2600".
- Shvetsov_ASh-82 specfuelcon "*M-82FN: 355 g/hp•h for take-off, 320 g/hp•hr at nominal power *M-82FNU: 360 g/hp•h for take-off, 325 g/hp•hr at nominal power *M-82T: 350 to 325 g/hp•h for take-off, 260 to 280 g/hp•hr at cruise power".
- Shvetsov_ASh-82 specpower "M-82FN: 29.84 kW/L , M-82FNU: 33.48 kW/L".
- Shvetsov_ASh-82 stroke "155.0".
- Shvetsov_ASh-82 supercharger "240000.0".
- Shvetsov_ASh-82 type Radial_engine.
- Shvetsov_ASh-82 type "14".
- Shvetsov_ASh-82 valvetrain "Pushrod, two valves per cylinder with sodium-cooled exhaust valve.".
- Shvetsov_ASh-82 weight "M-82-112 model: 860 kg , M-82FN model: 890 kg , M-82FNU model: 900 kg , M-82T model: 1,020 kg".
- Shvetsov_ASh-82 subject Category:Aircraft_air-cooled_radial_piston_engines.
- Shvetsov_ASh-82 subject Category:Aircraft_piston_engines_1940–1949.
- Shvetsov_ASh-82 subject Category:Shvetsov_aircraft_engines.
- Shvetsov_ASh-82 comment "The Shvetsov ASh-82 (M-82) is a 14-cylinder, two-row, air-cooled radial aircraft engine developed from the Shvetsov M-62. The M-62 was the result of development of the M-25, which was a licensed version of the Wright R-1820 Cyclone.".
- Shvetsov_ASh-82 label "ASz-82".
- Shvetsov_ASh-82 label "Shvetsov ASh-82".
- Shvetsov_ASh-82 label "Shvetsov ASh-82".
- Shvetsov_ASh-82 label "АШ-82".
- Shvetsov_ASh-82 label "シュベツォフ ASh-82".
- Shvetsov_ASh-82 sameAs Švecov_AŠ-82.
- Shvetsov_ASh-82 sameAs Shvetsov_ASh-82.
- Shvetsov_ASh-82 sameAs シュベツォフ_ASh-82.
- Shvetsov_ASh-82 sameAs ASz-82.
- Shvetsov_ASh-82 sameAs m.064qv9.
- Shvetsov_ASh-82 sameAs Q1050634.
- Shvetsov_ASh-82 sameAs Q1050634.
- Shvetsov_ASh-82 wasDerivedFrom Shvetsov_ASh-82?oldid=580639475.
- Shvetsov_ASh-82 depiction Aircraft_engine_Shvetsov_ASh-82T.JPG.
- Shvetsov_ASh-82 isPrimaryTopicOf Shvetsov_ASh-82.
