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ASTM D4809-18 establishes a precision test method for determining the heat of combustion of liquid hydrocarbon fuels using an oxygen bomb calorimeter. It is specifically designed for aviation turbine fuels where the permissible difference between duplicate determinations is of the order of 0.2 %. To attain this level of precision, the standard mandates strict adherence to all procedural details, as the error contributed by each individual measurement that affects the precision must be kept below 0.04 %.
Under normal conditions, this test method is directly applicable to a wide range of fuels including gasolines, kerosines, Nos. 1 and 2 fuel oil, Nos. 1-D and 2-D diesel fuel, and Nos. 0-GT, 1-GT, and 2-GT gas turbine fuels. The values stated in SI units are to be regarded as the standard for this test method.
The rigorous precision requirements of D4809-18 necessitate a comprehensive framework of supporting ASTM standards. These are referenced for the accurate determination of constituent elements like sulfur and hydrogen, as well as for the calibration and safe operation of the calorimetric apparatus. Strict adherence to these procedures ensures the integrity of the heat of combustion calculation.
| 📏 Key Parameter | 🎯 Specification / Requirement |
|---|---|
| Permissible Difference (Aviation Turbine Fuels) | 0.2 % |
| Maximum Error per Individual Measurement | 0.04 % |
| Primary Application Domain | Volatile and nonvolatile hydrocarbon fuels |
| 🟦 Referenced Standard | 📐 Function in D4809 Methodology |
|---|---|
| D240 | The predecessor test method; D4809 provides improved precision over this method. |
| D2622, D4294, D5453 | Methods for total sulfur determination needed for heat of combustion corrections. |
| D3701, D7171 | Low-resolution NMR spectroscopy methods for hydrogen content of aviation turbine and middle distillate fuels. |
| E1, E144 | Specifications for ASTM thermometers and safe practice for oxygen combustion vessels. |
D4809-18 offers significantly improved precision through the enhancement of calorimeter controls and temperature measurement devices, making it the preferred precision method for applications like aviation turbine fuel testing.
To achieve the overall precision of the method, the error contributed by each individual measurement (e.g., temperature, mass, time) must be kept strictly below 0.04 %.
It directly applies to aviation turbine fuels, gasolines, kerosines, Nos. 1 and 2 fuel oil, Nos. 1-D and 2-D diesel fuel, and Nos. 0-GT, 1-GT, and 2-GT gas turbine fuels.
The values stated in SI units are to be regarded as the standard for this test method. No other units of measurement are included in this standard.