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ASTM D5452-23 (Designation: 423/10) specifies the gravimetric determination of particulate contaminant in aviation turbine fuels. The fundamental principle involves passing a measured fuel sample through a pre-weighed test membrane filter under vacuum. To ensure accuracy, a control membrane is placed beneath the test membrane. The mass change difference between the test and control membranes, divided by the sample volume, identifies the contaminant level per unit volume. The values stated in SI units are to be regarded as the standard.
The test requires a membrane filtration apparatus, typically accommodating 47 mm or 37 mm diameter filters. The test membrane must have a pore size of 0.8 µm, while the control membrane is 0.45 µm. A stable vacuum source is essential. Sample containers must conform to the stringent cleanliness requirements of Practice D4306 to prevent trace contamination during handling and transport.
| 🟦 Component | 📏 Specification |
|---|---|
| Test Membrane Pore Size | 0.8 µm |
| Control Membrane Pore Size | 0.45 µm |
| Membrane Diameter | 37 mm or 47 mm |
| Vacuum Pressure | 70–85 kPa (10–12 psi) |
| Container Standard | Practice D4306 |
The filtration procedure requires rinsing the funnel assembly with clean solvent before introducing the sample. After filtering a known volume of fuel, the funnel is rinsed again to transfer all particles onto the membrane. Both the test and control membranes are then dried in a vacuum oven at 90°C and re-weighed. Accuracy demands an analytical balance capable of measuring to 0.1 mg.
| 📐 Step | 🎯 Key Parameter |
|---|---|
| Initial Weighing | Weigh test (0.8 µm) and control (0.45 µm) membranes |
| Filtration | Filter prescribed fuel volume through the stacked membranes |
| Drying | Vacuum oven drying to a stable weight |
| Final Weighing | Re-weigh test and control membranes |
| Calculation | Contaminant Level = (ΔWt – ΔWc) / Volume |
This standard provides a gravimetric laboratory filtration method for determining the mass of particulate contamination in a sample of aviation turbine fuel. It is a fundamental quality control test for fuel cleanliness used by fuel suppliers and testing laboratories.
The dual membrane system allows the control membrane to capture any extraneous weight changes from moisture absorption or solvent residues. This differential weighing technique isolates the true contaminant mass from environmental factors, improving accuracy.
Due to the flammability of aviation fuels, strict bonding and grounding procedures (as outlined in Guide D4865) must be followed to prevent static sparks. Additionally, the test should never be conducted in the presence of an open flame or ignition source.
The standard carries a dual designation (D5452-23 / 423/10), signifying it has been developed through a cooperative effort between ASTM and the Energy Institute (EI). It is technically equivalent to the IP standard, ensuring global consistency in test results for aviation fuel particulates.