The reliability and availability of AF depend on the quantity and composition of the components in the fuel. SAFs can be achieved by reducing or replacing unwanted components such as aromatics in conventional AF with strained PCHCs from PtL pathway [2] as blended fuel, and finally achieve 100% SAF. In the development phase of SAF, data obtained from measurements, testing, and computer modeling are employed to achieve insight into the desired properties from known structures of the compounds. For example, the net heat of combus�on (NHOC) of AF is crucial for understanding a fuel's energy content and performance characteris�cs for energy efficiency, flight range, and payload capacity of jets . The NHOC is categorized into gravimetric (NHOCG) and volumetric (NHOCV), and the former (NHOCG) is suitable for weight-limited aircraft, such as rockets and spacecraft.