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This test method, designated as D6446-01 (Reapproved 2006), provides an empirical procedure for estimating the net heat of combustion (specific energy) at constant pressure for aviation fuels. The estimation is based on fuel density, sulfur content, and hydrogen content, with results expressed in megajoules per kilogram. It is applicable only to liquid hydrocarbon fuels derived from conventional crude oil that conform to specifications for aviation turbine fuels, such as JP-5, JP-8, Jet A, and Jet A-1, as outlined in Note 1. The standard is under the jurisdiction of ASTM Committee D02 on Petroleum Products and Lubricants.
The empirical correlation requires accurate measurement of three key parameters. Density is determined using Test Methods D1217 or D4052. Sulfur content is measured via methods such as D129, D1266, or D2622. Hydrogen content is typically determined using Test Method D3701 (low-resolution NMR spectrometry). Alternative estimation approaches include Test Methods D1405, D3338, and D4529.
| 🟦 Parameter | 📐 Test Method |
|---|---|
| Density | D1217, D4052 |
| Sulfur Content | D129, D1266, D2622 |
| Hydrogen Content | D3701 |
The correlation used in this test method is derived from specific classes of fuels. The following table summarizes the fuel types and their governing specifications as per Note 1, along with their NATO codes.
| 🟦 Fuel Type | 📏 Specification | 🎯 NATO Code |
|---|---|---|
| JP-5, Avcat/FSII | MIL-DTL-5624, DEF STAN 91-86 | F-44 |
| JP-8, Avtur/FSII | MIL-DTL-83133, DEF STAN 91-87 | F-34 |
| Jet A, Jet A-1, Avtur | D1655, DEF STAN 91-91 | F-35 |
Users should recognize that this test method is purely empirical and estimates can be in error for individual fuels, even within these defined classes. It is critical to adhere to the fuel specifications listed to ensure reasonable accuracy.
This standard provides an empirical method to estimate the net heat of combustion (specific energy) of aviation fuels from measurements of density, sulfur content, and hydrogen content.
The net heat of combustion is expressed in SI units as megajoules per kilogram (MJ/kg) at constant pressure.
Alternative estimation methods include Test Methods D1405, D3338, and D4529, which can be used for similar purposes.
No, it is limited to liquid hydrocarbon fuels derived from conventional crude oil that meet specific aviation turbine fuel specifications, such as those listed in Note 1 (e.g., JP-5, JP-8, Jet A, Jet A-1).