HIGH OCTANE UNLEADED AVIATION GASOLINE

摘要

High octane unleaded aviation fuel compositions having a CHN content of at least 97.2wt%, less than 2.8 wt% of oxygen content, a T10 of at most 75°C, T40 of at least 75° C, a T50 of at most 105° C, a T90 of at most 135°C, a final boiling point of less than 210°, an adjusted heat of combustion of at least 43.5 MJ/kg, a vapor pressure in the range of 38 to 49 kPa is provided.