Bedrock 3D Standard Black TPU 64D Black
MaterialID MAT0253

3DPIceland Labs
Generated with 3DPIceland Engineering Platform v70.0.4 DIRECT-IMPACT-METHODOLOGY - Izod and Charpy Methodology
2026-10-04 18:12:06
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0/8
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42.39
Engineering profile
Recommended applications
- Application guidance awaits sufficient measured evidence and approved score references
Measured strengths
- No scored strength is available yet.
Limitations
- No scored limitation can be established from the available evidence.
Engineering trade-offs
- Complete scoring evidence and approved method references are required before assessing an overall balance of properties.
Base-material printing guidance
| Guidance | Minimum | Recommended | Maximum | Unit |
|---|---|---|---|---|
| Nozzle temperature | 220 | 225 | 260 | °C |
| Bed temperature | 65 | 65 | 65 | °C |
| Print speed | 11 | 30 | 30 | mm/s |
| Cooling | 65 | 65 | 65 | % |
| Guidance | Value | Unit |
|---|---|---|
| Cooling guidance | High | |
| Drying temperature | 65 | °C |
| Drying time | 8 | hours |
| Enclosure | Not required | |
| Printer / G-code reference | PrusaCoreOneL | |
| Slicer profile reference | Prusament TPU 95A |
Print workflow checks
- Confirm nozzle temperature, bed temperature, speed, cooling and drying requirements from the manufacturer profile or spool label.
- Print a small validation part before committing to a long, costly or safety-relevant print.
- Orient the part so the governing load does not rely on an unverified or weak engineering axis.
- Flexible family: validate extrusion path, retraction and speed conservatively on the actual printer.
- Layer-adhesion evidence is weak; avoid critical Z-axis loading without additional validation.
- Repeatability is low on the internal scale; run extra validation specimens before relying on the profile.
Decision guidance
- Overall suitability is unavailable until the required measurements and method references are complete.
Stronger same-family alternatives
| MaterialID | Material | Manufacturer | Overall | Tensile | Impact | Izod | Charpy |
|---|
Testing methodology · Download PDF
Flexible Material Testing
Comparative in-house measurements; n = independent specimens. Separate test groups; Overall unchanged.
| Method | Result | Condition | Mean | n | SD | CV % | Range | Not reached |
|---|---|---|---|---|---|---|---|---|
| eaacea91 | Apparent Compressive Stress at 20% Strain (MPa) | 10 s hold · 2 mm displacement · cycle 1 | 6.885 | 9 | 0.133 | 1.934 | 6.728–7.074 | 0 |
| eaacea91 | Apparent Compressive Stress at 20% Strain (MPa) | 30 s hold · 2 mm displacement · cycle 1 | 6.352 | 9 | 0.128 | 2.016 | 6.193–6.571 | 0 |
| eaacea91 | Compression Force at 20% Strain (N) | 10 s hold · 2 mm displacement · cycle 1 | 438 | 9 | 8.471 | 1.934 | 428–450 | 0 |
| eaacea91 | Compression Force at 20% Strain (N) | 30 s hold · 2 mm displacement · cycle 1 | 404.111 | 9 | 8.146 | 2.016 | 394–418 | 0 |
| eaacea91 | Force reduction from 10 s to 30 s at 20% Strain (%) | first compression only · 2 mm displacement | 7.738 | 9 | 0.443 | 5.731 | 7.111–8.372 | 0 |
| eaacea91 | Force retention at 20% Strain (%) | 10–30 s · 2 mm displacement · cycle 1 | 92.262 | 9 | 0.443 | 0.481 | 91.628–92.889 | 0 |
| eaacea91 | Residual height loss after recovery (%) | 20% compression · 30 s compressed hold · 60 s rest · 10 mm initial height · cycle 1 | 1.956 | 9 | 0.124 | 6.321 | 1.8–2.2 | 0 |
| ed381ba8 | Shore A Hardness (Shore A) | 10 s reading · 8 mm | 91.9 | 1 | — | — | 91.9–91.9 | 0 |
Shore location statistics
Within each specimen; specimen numbers are local to each test group. SD uses the sample formula. These readings do not increase independent n.
| Method | Scale | Condition | Specimen | Readings | Mean | Location SD | Location CV % |
|---|---|---|---|---|---|---|---|
| ed381ba8 | Shore A Hardness | 10 s reading · 8 mm | 1 | 5 | 91.9 | 4.561 | 4.963 |
Score policy engineering-score-v70-1: Overall requires tensile, stiffness, consistency, layer adhesion and the Izod/Charpy impact family, each with equal weight. Both impact methods and configured versioned references are required. Missing results and unconfigured scores remain n/a. Legacy Impact is historical only; thermal remains separate. Engineering-axis counts describe displayed evidence, not Overall completeness.