Statements (61)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turboshaft engine
|
| gptkbp:application |
civil and military helicopters
|
| gptkbp:compressionRatio |
16:1
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:design |
3,000 hours
|
| gptkbp:designedBy |
Klimov
|
| gptkbp:diameter |
600 mm
|
| gptkbp:drivetrain |
reduction gearbox
|
| gptkbp:emissionsStandard |
compliant with standards
|
| gptkbp:engine |
300 kg
|
| gptkbp:engineConfiguration |
V-type
|
| gptkbp:exhaustSystem |
single exhaust
|
| gptkbp:firstFlight |
1970
|
| gptkbp:fuelCapacity |
200 kg/h
|
| gptkbp:fuelType |
kerosene
annular combustion chamber |
| https://www.w3.org/2000/01/rdf-schema#label |
TV3-117 engine
|
| gptkbp:launchSite |
electrical starter
|
| gptkbp:length |
1,200 mm
|
| gptkbp:maintenance |
1,000 hours
|
| gptkbp:manufacturer |
Klimov
|
| gptkbp:noise_level |
low
|
| gptkbp:operationalStatus |
up to 1,000 °C
|
| gptkbp:powerOutput |
1,250 kW
|
| gptkbp:powers |
1,700 shp
|
| gptkbp:propulsion |
1,700 lbf
5.67 kW/kg |
| gptkbp:reliability |
high
|
| gptkbp:services |
5,000 m
|
| gptkbp:type |
twin-shaft
|
| gptkbp:usedIn |
gptkb:Kamov_Ka-32
gptkb:Mil_Mi-17 Mil Mi-8 |
| gptkbp:variant |
TV3-117V
TV3-117VMA TV3-117VM TV3-117VMA-SB TV3-117VMA-SB3 TV3-117VMA-SB3M TV3-117VMA-SB3M1 TV3-117VMA-SB3M10 TV3-117VMA-SB3M11 TV3-117VMA-SB3M12 TV3-117VMA-SB3M13 TV3-117VMA-SB3M14 TV3-117VMA-SB3M15 TV3-117VMA-SB3M16 TV3-117VMA-SB3M17 TV3-117VMA-SB3M18 TV3-117VMA-SB3M19 TV3-117VMA-SB3M2 TV3-117VMA-SB3M20 TV3-117VMA-SB3M3 TV3-117VMA-SB3M4 TV3-117VMA-SB3M5 TV3-117VMA-SB3M6 TV3-117VMA-SB3M7 TV3-117VMA-SB3M8 TV3-117VMA-SB3M9 |
| gptkbp:weight |
about 300 kg
|