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ASTM D3171-22, approved for use by U.S. Department of Defense agencies, provides two distinct approaches for determining the constituent content of composite materials. Test Method I physically removes the matrix via one of eight procedures: chemical digestion (Procedures A–F), ignition (Procedure G), or carbonization (Procedure H), leaving the reinforcement essentially unaffected. A specific correction procedure is included to address minor changes to the reinforcement during processing. Test Method II calculates constituent content for laminates where the fiber areal weight is known or tightly controlled.
Specimens must be properly prepared and conditioned. The standard references Test Method D5229/D5229M for moisture conditioning of polymer matrix composites. Density measurements, critical for converting weight fractions to volume fractions, must be conducted following Test Methods D792 (displacement) or D1505 (density gradient). All values are stated in SI units per Section 1.2.
Test Method I assumes the reinforcement is essentially unaffected by the removal medium, whether chemical, thermal (ignition), or carbonization. Procedures A through F utilize chemical digestion; Procedure G removes the matrix by ignition in a furnace; Procedure H uses carbonization in a furnace. The method allows direct calculation of fiber or matrix content (by weight or volume) and the percentage of void volume.
Test Method II is applicable only to laminate materials of known fiber areal weight. It calculates reinforcement or matrix content and the cured ply thickness based on the measured thickness of the laminate. An important caveat from Section 1.1.4 is that the presence of voids is not measured, and Eq 15 and Eq 16 strictly assume zero void content to perform the calculation.
The primary outputs of these tests include fiber volume fraction (Vf), matrix volume fraction (Vm), fiber weight fraction (Wf), matrix weight fraction (Wm), and void volume fraction (Vv) for Test Method I. For Test Method II, the cured ply thickness is a crucial calculated property. While these methods primarily target two-part composite systems, special provisions in Section 1.1.1 allow extension to filled systems, though not all constituent fractions can be determined in every case.
Terminology is harmonized with D3878 (Composite Materials), D883 (Plastics), and E12. Precision and bias must be reported following Practice E177.
| 🟦 Procedure | 📏 Removal Method | 🎯 Suggested Matrix Systems |
|---|---|---|
| A – F | Chemical Digestion | Polymer or Metal Matrices |
| G | Ignition (Furnace) | Polymer Matrices |
| H | Carbonization (Furnace) | Polymer Matrices |
| 🟦 Standard | 📏 Title / Purpose |
|---|---|
| D792 | Density and Specific Gravity of Plastics by Displacement |
| D1505 | Density of Plastics by the Density-Gradient Technique |
| D3878 | Terminology for Composite Materials |
| D5229/D5229M | Moisture Absorption Properties and Equilibrium Conditioning |