RU / EN
Technical Specifications 38.101299-90
IPM-10 is a synthetic hydrocarbon oil with a complex of highly effective additives.
IPM-10 is applied for the heat-stressed gas-turbine engines of military and civil aviation with the outlet temperature up to 200°C (civil aviation aircrafts IL-62, IL-86, Tu-134, Tu-154, Yak-42, An-12 an-24, an-26, an-30), aerial power units (APU) TA-6(A), TA-8, TA-12, TA-8V, turboalternator (THU), and gas-pumping units driven by the aircraft engine.
Properties:
| Indicator name | Norms |
| Kinematic viscosity, mm2/s (St): | |
| at 100°C, not less | 3,0 |
| at - 40°C, not more | 3000 |
| The flash point determined in open crucible °C, not below | 190 |
| Pour point, °C, not above | -50 |
| Thermal-oxidative stability at 200°C for 50 hours and the air 3 dm3/h: | |
| a) mass fraction of precipitate insoluble in isooctane, %, not more | 0,35 |
| b) acid number after oxidation, mg KOH/g oil not more than | 8 |
| C) kinematic viscosity after oxidation: | |
| at - 40°C, mm2/s (St), not more | 5000 |
| at 100°C, mm2/s (St), not more | 5,0 |
| d) weight corrosion index after oxidation, mg/cm2, on LP: | |
| alloy wrought aluminium brand AK4 (GOST 4784-74), max. | Lack |
| copper grade M1 or M2(GOST 859-78), max. | 0,2 |
| steel SH-15 (GOST 801-78) | Lack |
| Warranty period of storage | 5 years |