MS-500V-S
The MS-500V-S family engines are designed to power aircraft of various purpose and allow achieving high economic performance during commercial service. Two engine designs (with a shaft looking forward and aft) have been developed in order to ensure an optimal engine configuration for various airplane types. |
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Engine main advantages
- simple and efficient design
- high reliability
- low specific fuel consumption
- high stability of characteristics during operation
- compliance with environmental requirements
- high service life and calendar life
- simple and convenient maintenance
- cheap life cycle
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Basic specifications:
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МS-500V-S
МS-500V-02S/SТ
МS-500V-04S/SE/SBE |
МS-500V-01S
МS-500V-03S
МS-500V-05S/SE/SBE |
| Emergency power with one engine inoperative (OEI) (H=0, Vfl=0, ISA) |
| Propeller shaft power, hp (kW) |
950 (699) |
1,200 (883)...1,140 (838) |
| maintained to tamb, °C |
+15 |
+15...+25 |
| Take-off power (H=0, Vfl=0, ISA): |
| Propeller shaft power, hp (kW) |
950 (699)...810 (596) |
1,050 (772)...900 (662) |
| maintained to tamb, °C |
+15...+30 |
+22...+41 |
| Maximum continuous power (H=0, Vfl=0, ISA) |
| Propeller shaft power, hp (kW) |
720 (530) |
780 (574) |
| maintained to tamb, °C |
+20 |
+30 |
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Cruise power rating (H=3000, V=407 km/h, ISA):
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| Propeller shaft power, hp (kW) |
670 (493) |
670 (493) |
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Specific fuel consumption, kg/(hp•h)
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0.240 |
0.238 |
| Ground idle (H=0, Vfl=0, ISA) |
| Propeller shaft power, hp (kW) |
65 (48) |
65 (48) |
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