| 摘要 |
High octane unleaded aviation fuel composition having high aromatics content and CHN content of at least 97.8wt%, less than 2.2 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 190°C, 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. |
