The ASTM D7566-24 standard specification defines the requirements for aviation turbine fuel containing synthesized hydrocarbons. This document outlines the physical and chemical properties necessary to ensure the safe and efficient operation of jet engines when using this type of fuel. Developed by the American Society for Testing and Materials (ASTM), it is intended for use in aviation applications where synthetic fuels are utilized as an alternative or supplement to traditional petroleum-based aviation turbine fuels. The specification includes criteria related to distillation characteristics, cold-soak precipitation temperature, thermal oxidative stability, water separability, and other key attributes that impact fuel performance and handling.
*** Please note: This description may not be accurate, please refer to the official documentation.
Copyright ©2025 All Rights Reserved