Description
Oil MS-8p TPO 38.01163-78 for gas turbine engines subsonic and supersonic aircraft in which the oil outlet temperature from the engine is not more than 150 ° C.
Applications
Oil MS-8p most widely used oil-based oil with a highly complex additives. Produced from West-Siberian and mixtures West Siberian and the Ural crude oils. Oil MS-8p used in the composition maslosmesey with aviation oil MS-20 (in a ratio of 25:75, 50:50 and 75:25) in turboprop engines, as well as for preserving the oil systems of aircraft engines. Used in the ship’s gas turbines and gas compressor units.
Oil MS-8p designed to replace oils MK-8 and MK 8n, it greatly surpasses them on a number of operational parameters, in particular low temperature toughness, thermal oxidative stability, resource work.
Specifications
Indicator | Norm |
Kinematic viscosity mm2 /s (cSt): | |
at 50 ° C, at least | 8,0 |
at minus 40 ° C, no more than | 4000 |
Flash point open cup, ° C, min | 145 |
Pour Point, ° C, max | -55 |
thermooxidative stability at 150 ° C for 50 hours: | |
a) kinematic viscosity at 50 ° C after oxidation cSt, not more than | 10 |
b) a kinematic viscosity at -40 ° C after oxidation cSt, not more than | 5500 |
a) acid number after oxidation, mg KOH per 1 g of oil, not more than | 0,7 |
g) the mass fraction of the precipitate after oxidation,%, not more than | 0,15 |
d) corrosion on wafers after oxidation, mg /cm2 and not more than: | |
steel SH-15 according to GOST 801-60 | no |
copper M1 or M2 as per GOST 859-66 | ± 0,2 |
aluminum alloy AK-4 in accordance with GOST 4784-74 | no |
Guaranteed shelf life | 5 years |
Additional information
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