Submitted:
30 January 2026
Posted:
02 February 2026
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Abstract
Keywords:
1. Introduction
1.1. Importance of Hermeticity in 3D-Printed Enclosures
1.2. Effective Leak Detection Techniques
1.3. Knowledge Gap in Application of Vacuum Leak Testing
1.4. Research Objectives
| Objective | Description / Detail |
|---|---|
| Methodological Development | To establish a robust and rigorously reproducible experimental protocol for the vacuum leak testing of 3D-printed enclosures, specifically tailored to address the unique geometrical and material characteristics of architectural façade components, ensuring precision and replicability. |
| Performance Evaluation | To quantitatively assess the diagnostic capabilities and reliability of the adapted vacuum leak detection method, evaluating its sensitivity in discerning micro-leaks and macro-leaks across various sizes and locations within complex internal structures of additively manufactured components. |
| Procedural Framework | To formulate a comprehensive procedural framework that facilitates the seamless integration of non-destructive evaluation (NDE) protocols [31] into the quality assurance processes during both the manufacturing and assembly stages of 3D-printed architectural elements, aiming for long-term hermetic integrity. |
| Influence Analysis | To critically investigate the intricate interdependencies between design parameters, inherent material properties, and manufacturing tolerances on the achieved hermeticity and subsequent test outcomes of the assembled enclosures, informing future optimization of design and fabrication strategies. |
1.5. Structure of the Manuscript
2. Materials and Methods
2.1. Materials
| Filament Type | Color | Description |
|---|---|---|
| PLA Basic | Black | Polylactic Acid |
| PLA Aero | Light-Gray | Foaming grade of Polylactic Acid, Bambu PLA Aero |
| PETG | Clear | ReFill PETG 3D-Printing material by Formfutura |
| PET-CF | Black | Bambu PET-CF |
2.2. Printing Parameters (Slicer Values)
| Filament | PET-CF | PETG | PLA-Aero | PLA |
|---|---|---|---|---|
| Vendor | Bambu Lab | Form Futura | Bambu Lab | Bambu Lab |
| Default Color | Black | Translucent | Black | |
| Filament Diameter Flow Ratio |
1.75 mm | 1,75 mm | 1.75 mm | 1.75 mm |
| 1.0 | 0,95 | 0,6 | 0,98 | |
| Density | 1.29 g/cm³ | 1.25 g/cm³ | 1.21 g/cm³ | 1.26 g/cm³ |
| Shrinkage | 100% | 100% | 100% | 100% |
| Recommended Nozzle Temperature | Min: 260 °C, Max: 290 °C | Min: 230 °C, Max: 270 °C |
Min: 210 °C, Max: 260 °C |
Min: 190 °C, Max: 240 °C |
| Print Temperature | Initial Layer: 270 °C |
Initial Layer: 250 °C |
Initial Layer: 220 °C |
Initial Layer: 220 °C |
| Other Layers: 270 °C | Other Layers: 245 °C |
Other Layers: 220 °C |
Other Layers: 220 °C |
|
| Textured PEI Plate | Initial Layer: 100 °C | Initial Layer: 70 °C |
Initial Layer: 65 °C | Initial Layer: 65 °C |
| Other Layers: 100 °C | Other Layers: 70 °C | Other Layers: 65 °C | Other Layers: 65 °C |
|
| Max Volumetric Speed | 8 mm³/s | 6 mm³/s | 6 mm³/s | 21 mm³/s |
| Ramming Volumetric Speed | -1 mm³/s | -1 mm³/s | -1 mm³/s | -1 mm³/s |
| Nozzle Diameter | 0.4 mm | 0.4 mm | 0.4 mm | 0.4 mm |
| Layer Height | 0.12 mm | 0.12 mm | 0.12 mm | 0.12 mm |
| Initial Layer Height | 0.2 mm | 0.2 mm | 0.2 mm | 0.2 mm |
| Line Width | Default: 0.42 mm Initial Layer: 0.5 mm |
Default: 0.42 mm Initial Layer: 0.5 mm |
Default: 0.42 mm Initial Layer: 0.5 mm |
Default: 0.42 mm Initial Layer: 0.5 mm |
| Wall Loops | 10 | 10 | 10 | 10 |
| Top Surface Pattern | Concentric | Concentric | Concentric | Concentric |
| Top Shell Layers | 35 | 35 | 35 | 35 |
| Top Shell Thickness | 0,6 mm | 0,6 mm | 0,6 mm | 0,6 mm |
| Top Paint Penetration Layers | 10 | 10 | 10 | 10 |
| Bottom Surface Pattern | Rectilinear | Rectilinear | Rectilinear | Rectilinear |
| Bottom Shell Layers | 20 | 20 | 20 | 20 |
| Bottom Shell Thickness | 0 mm | 0 mm | 0 mm | 0 mm |
| Bottom Paint Penetration Layers |
10 | 10 | 10 | 10 |
| Internal solid infill pattern |
Rectilinear | Rectilinear | Rectilinear | Rectilinear |
| Sparse Infill Density | 90% | 90% | 90% | 90% |
| Infill/ Wall Overlap | 90% | 90% | 90% | 90% |
| Sparse Infill Pattern | Gyroid | Gyroid | Gyroid | Gyroid |
| Scarf Steps | 10% | 10% | 10% | 10% |
| Initial Layer Speed | 50 mm/s | 50 mm/s | 50 mm/s | 50 mm/s |
| Other Layers Speed | Outer Wall: 60 mm/s Inner Wall: 150 mm/s |
Outer Wall: 60 mm/s Inner Wall: 150 mm/s |
Outer Wall: 60 mm/s Inner Wall: 150 mm/s |
Outer Wall: 60 mm/s Inner Wall: 150 mm/s |
| Travel Speed | 700 mm/s | 700 mm/s | 700 mm/s | 700 mm/s |
| Acceleration | Normal Printing: 4000 mm/s² Travel: 10000 mm/s² Initial Layer Travel: 6000 mm/s² Outer Wall: 2000 mm/s² |
Normal Printing: 4000 mm/s² Travel: 10000 mm/s² Initial Layer Travel: 6000 mm/s² Outer Wall: 2000 mm/s² |
Normal Printing: 4000 mm/s² Travel: 10000 mm/s² Initial Layer Travel: 6000 mm/s² Outer Wall: 2000 mm/s² |
Normal Printing: 4000 mm/s² Travel: 10000 mm/s² Initial Layer Travel: 6000 mm/s² Outer Wall: 2000 mm/s² |
| Bed Adhesion – Skirt Loops |
0 | 0 | 0 | 0 |
| Support Type | Normal (Auto) | Normal (Auto) | Normal(Auto) | Normal (Auto) |
| Brim Type | Outer Brim | Outer Brim | Outer Brim | Outer Brim |
| Brim Width | 5 mm | 5 mm | 5 mm | 5 mm |
| Filament for Supports | Support/Raft Base | Support/Raft Base | Support/Raft Base | Support/Raft Base |
| G-code Output | Reduce Infill Retraction | Reduce Infill Retraction | Reduce Infill Retraction | Reduce Infill Retraction |
| Special Mode – Slicing Mode |
Regular | Regular | Regular | Regular |
| Fuzzy Skin Thickness | 0.3 mm | 0.3 mm | 0.3 mm | 0.3 mm |
| Fuzzy Skin Point Distance |
0.8 mm | 0.8 mm | 0.8 mm | 0.8 mm |
2.3. Experimental Procedure
2.4. Experimental Protocol
2.4.1. Initial Setup
2.4.2. Test Planning
| Experimental chamber type |
Initial pressure at t=0 (bar) | Final pressure at t=Duration (bar) | Monitoring duration (min) |
Pressure decay (bar) |
|---|---|---|---|---|
| PET-CF | 0.25 | 0,25 | 20 | 0,00 |
| PET-CF | 0.25 | 0,25 | 40 | 0,00 |
| PET-CF |
0.25 | 0,25 | 60 | 0,00 |
| PET-CF | 0,50 | 0,50 | 20 | 0,00 |
| PET-CF | 0,50 |
0,50 | 40 | 0,00 |
| PET-CF | 0,50 | 0,50 | 60 |
0,00 |
| PETG | 0.25 | 0,00 | 20 | 0,25 |
| PETG | 0.25 | 0,00 | 40 |
0,25 |
| PETG | 0.25 | 0,00 | 60 | 0,25 |
| PETG | 0.50 | 0,00 | 20 |
0,50 |
| PETG | 0.50 | 0,00 | 40 | 0,50 |
| PETG | 0.50 | 0,00 | 60 |
0,50 |
| PLA-Aero | 0.25 |
0,00 | 20 | 0,25 |
| PLA-Aero | 0.25 |
0,00 | 40 | 0,25 |
| PLA-Aero | 0.25 |
0,00 | 60 | 0,25 |
| PLA-Aero | 0.50 |
0,00 | 20 | 0,50 |
| PLA-Aero | 0.50 |
0,00 | 40 | 0,50 |
| PLA-Aero | 0.50 |
0,00 | 60 | 0,50 |
| PLA | 0.25 | 0,20 | 20 |
0,05 |
| PLA | 0.25 | 0,16 | 40 |
0,09 |
| PLA | 0.25 | 0,13 | 60 | 0,12 |
| PLA | 0.50 | 0,43 | 20 | 0,07 |
| PLA | 0.50 | 0,35 | 40 | 0,15 |
| PLA | 0.50 | 0,30 | 60 | 0,20 |
2.5. Analysis and Replicability of the Study
2.5.1. Data Collection and Archiving
2.5.2. Instruments, Calibration and Traceability
2.5.3. Data Processing and Analysis Workflow
2.5.4. Statistical Methods and Uncertainty Quantification
2.5.5. Quality Control and Validation
2.5.6. Reproducibility Checklist and Required Reporting
2.5.7. Access, Licensing and Ethical Considerations
2.5.8. Limitations and Recommended Caution for Replicators
2.5.9. Contact and Support
3. Results
3.1. Data Completeness and Preprocessing
3.2. Overview of Pressure-Decay Behaviour by Material
3.3. Replicate Variability and Instrument Uncertainty
- PET-CF: SD ≈ 0.00 bar (within gauge resolution) after baseline correction.
- PETG and PLA-Aero: SD small relative to full decay magnitude; all replicates showed full loss within the first interval.
- PLA: SD ranged between 0.01 and 0.03 bar across conditions. Given the QS30190 gauge precision of ±0.05 bar, the observed PLA variability is within an expected combined measurement and sample variability envelope but consistent and repeatable across replicates. Uncertainty propagation combined instrument precision, chamber volume uncertainty (estimated ±2%), and baseline subtraction variance to produce combined standard uncertainties reported below for leak-rate estimates.
3.4. Quantitative Leak-Rate Estimates and Uncertainty
- PET-CF
- PETG
- PLA-Aero
- PLA (standard)
- − 20 min: 0.05/20 = 0.0025 ± 0.0006 bar·min⁻¹
- − 40 min: 0.09/40 = 0.00225 ± 0.0005 bar·min⁻¹
- − 60 min: 0.12/60 = 0.0020 ± 0.0005 bar·min⁻¹
- − Mean ≈ 0.00225 ± 0.0006 bar·min⁻¹
- − 20 min: 0.07/20 = 0.0035 ± 0.0008 bar·min⁻¹
- − 40 min: 0.15/40 = 0.00375 ± 0.0009 bar·min⁻¹
- − 60 min: 0.20/60 = 0.00333 ± 0.0008 bar·min⁻¹
- − Mean ≈ 0.00353 ± 0.0009 bar·min⁻¹
3.5. Time-Dependent Behaviour and Linearity
3.6. Statistical Comparisons
- PET-CF vs. PETG: statistically significant difference in pressure-decay (p < 0.01).
- PET-CF vs. PLA-Aero: statistically significant (p < 0.01).
- PET-CF vs. PLA: statistically significant (p < 0.05).
- PLA vs. PETG / PLA-Aero: statistically significant differences (p < 0.01). These results confirm that material identity is a significant predictor of measured pressure decay under the experimental protocol.
3.7. Correlation with Mass and Microscopy
3.8. Visualisation and Insertion Points for Figures

3.9. Ancillary Checks and Control Runs
3.10. Limitations of the Measured Results
3.11. Key Findings and Implications from Results
- PET-CF demonstrates effective hermetic performance under the tested printing parameters and geometry, retaining vacuum for at least 60 min at 0.25 and 0.50 bar.
- PETG and PLA-Aero, as printed, fail to retain the applied vacuum and equilibrate rapidly with atmosphere, indicating substantial leakage pathways or insufficient sealing for the tested geometry and settings.
- PLA shows intermediate behaviour with reproducible, time-dependent decay and higher absolute loss at greater initial vacuum; this suggests that targeted parameter optimization or post-processing could improve hermeticity but that as-printed PLA is not as robust as PET-CF for vacuum retention.
4. Discussion
4.1. Interpretation of Principal Results
4.2. Mechanistic Interpretation and Microstructural Evidence
- Micro-channels from incomplete inter-layer fusion: PLA samples showed intermittent inter-layer gaps and micro-porosity consistent with slow permeation and progressive pressure loss. The near-linearity of PLA decay suggests diffusive/transient flow through many small tortuous channels rather than a single dominant macroscopic breach.
- Localized macroscopic defects or poor perimeter sealing: PETG and PLA-Aero exhibited features consistent with larger surface defects or seam discontinuities that allow rapid bulk flow (convective equilibration) and therefore step-like pressure decay within the first measurement interval.
- Material-dependent permeability and reinforcement effects: PET-CF (carbon-fiber reinforced PET) likely benefits from changes in melt rheology, particle-induced densification of deposited roads, or filler-induced tortuosity that reduce effective gas permeability and improve layer consolidation. Carbon fibers may stiffen the extrudate, reduce shrinkage-induced separations, or alter cooling rates favorably for inter-layer adhesion.
4.3. Relation to Existing Literature and Standards
4.4. Statistical and Methodological Considerations
- Sensitivity and detection limits: The QS30190 gauge resolution (±0.05 bar) sets a practical detection threshold. PET-CF’s “zero” decay must be interpreted as “no measurable decay above the detection threshold and baseline-corrected system leakage” rather than absolute zero leak-rate. For small leaks near the gauge resolution, uncertainty propagation and confidence intervals are critical when comparing materials.
- Temporal resolution: The 20 min first sampling interval is insufficient to resolve leak kinetics faster than that interval. For PETG and PLA-Aero, reported leak-rate proxies are lower bounds; the true leak dynamics likely occur on timescales shorter than 20 min. Future experiments using continuous logging or shorter sampling intervals (e.g., 1–5 min) would allow more accurate kinetic descriptions.
- Replication and reproducibility: Triplicate runs produced consistent materials’ rankings, indicating robust reproducibility under the tested protocol. However, inter-batch filament variability and printer-to-printer differences remain potential sources of broader variance.
4.5. Practical Implications for Design, Manufacturing and QC
- Material selection: PET-CF, when printed with the tested parameters, is a strong candidate for vacuum-retention components in façade systems, subject to extended environmental testing. PETG and PLA-Aero require additional interventions—either process adjustments (parameter tuning, orientation changes) or post-print sealing—before use in hermetic applications.
- Design-for-hermeticity: Designers should minimize through-thickness seam lengths in critical sealing surfaces, include mating features that allow compression gaskets or adhesive beads, and orient parts to reduce continuous vertical layer seams across sealing planes.
- Slicer and process controls: Recommendations include increasing extrusion temperature (within safe filament limits) to promote inter-diffusion, decreasing layer height to increase road overlap, increasing perimeters/wall counts and flow multiplier to reduce internal porosity, and slowing outer-wall speeds to ensure consistent deposition.
- Post-processing and sealing: Practical measures include epoxy/urethane coatings, parylene deposition, solvent smoothing (where chemically compatible), thermal annealing to relieve residual stresses and improve layer fusion, and localized laser/IR welding for critical joints.
- Quality assurance: Implement in-line pressure-decay screening for production lots, with blank-run baselines and leaky-reference controls. Define application-specific acceptance thresholds (e.g., maximum allowable decay at 60 min) that reflect thermal insulation or sensor reliability requirements of façade elements.
4.6. Safety, Regulatory and Durability Considerations
- Fire and building codes: Any material or post-processing used for façades must comply with local fire safety and building regulations (flammability, smoke toxicity, structural performance). Coatings and adhesives used to improve hermeticity must be assessed for fire behaviour and chemical compatibility with substrate materials.
- Long-term durability: Environmental exposures (UV, freeze-thaw cycles, humidity, pollutants) [32] may degrade polymer matrices or coatings, producing new leak paths over time. Accelerated ageing studies (UV, hygrothermal cycling, mechanical fatigue) are necessary to evaluate lifecycle hermeticity.
- Sensor and embedded system reliability: For housings containing electronics or sensors, hermetic failure modes (moisture ingress, condensation) may be especially critical. Sealing strategies should be validated under combined environmental and electrical testing relevant to the sensor lifetime.
4.7. Limitations and Caveats (Expanded)
- Gauge and method limits: The pressure gauge’s resolution limited sensitivity to very small leaks; helium mass spectrometry or fine vacuum instrumentation is recommended for quantifying leaks below current detection limits.
- Geometry and assembly complexity: The scoped geometry was a simple cube; real façade components will include seams, fasteners, multi-part assemblies, and larger volumes where leak paths and mechanical stresses differ.
- Single print profile set: Only one primary set of slicer settings was tested per material. Optimized profiles may change hermetic outcomes substantially; thus, these results are conditional on the tested profiles.
- Environmental representativity: Tests were performed in stable laboratory conditions; field conditions impose multi-factor stresses not captured here.
4.8. Recommendations for Further Research (Specific Experiments)
- High-resolution leak kinetics: Use continuous pressure logging (sampled at ≥1 Hz) and/or tracer-gas (helium) mass-spectrometry leak detection to accurately characterize fast leak events and to convert decay into standardized leak-rate units (e.g., mbar·L·s⁻¹ or Pa·m³·s⁻¹).
- Parametric print study: Conduct a factorial study varying nozzle temperature, layer height, flow rate, wall count, print speed, orientation, and cooling to quantify parameter sensitivities for hermeticity per material.
- Post-processing efficacy: Systematically evaluate surface coatings (types, thicknesses), thermal annealing schedules, solvent smoothing, and welding approaches for leak reduction and durability under accelerated ageing.
- Multi-part assembly testing: Evaluate hermetic performance of assembled components (mating surfaces, adhesives, gaskets, fasteners) under mechanical loading and thermal cycling.
- Long-term environmental trials: Outdoor exposure tests and accelerated ageing to assess retention of hermeticity over expected façade lifetimes.
- Life-cycle and cost-benefit analysis: Analyze cost, manufacturability, repairability and environmental impact of sealing strategies compared to conventional manufacturing methods for façade components.
4.9. Implementation Roadmap for Industry Uptake
- Short term: Adopt PET-CF for prototyping vacuum-retentive cells and introduce batch-level pressure-decay QC. For PETG/PLA-Aero, mandate post-print sealing or perform parameter re-qualification before use.
- Medium term: Develop optimized print profiles and standardized sealing processes validated by accelerated ageing tests; integrate in-process inspection (e.g., acoustic/thermal imaging) for early defect detection.
- Long term: Engage with standards bodies to define application-specific acceptance criteria for 3D-printed hermetic enclosures in architectural contexts and pursue certification pathways for façade products incorporating printed vacuum cells.
4.10. Concluding Remarks
5. Conclusions
- Method validation: The adapted pressure-decay protocol (baseline-corrected, ASTM F2095 / BS EN 1779 framework) proved an effective, low-cost screening tool for comparing hermetic performance across FDM materials and print settings for 30×30×30 mm test chambers. It reliably separated clearly hermetic, partially hermetic, and non-hermetic behaviours under laboratory conditions.
- PET-CF: Demonstrated no measurable pressure decay over 60 min at 0.25 and 0.50 bar within the limits of the instrumentation. This indicates good as-printed hermetic performance for the tested geometry and slicer profile.
- PLA (standard): Exhibited reproducible, time-dependent leakage with near-linear cumulative decay; higher initial vacuum produced larger absolute decay and slightly higher mean leak-rates.
- PETG and PLA-Aero: Showed rapid, essentially complete loss of the applied vacuum within the first 20-min interval, consistent with macroscopic leak paths or poor sealing as printed.
- Mechanistic insight: Microscopy and comparative mass data point to inter-layer fusion quality, perimeter/seam integrity and material rheology (including filler effects for PET-CF) as primary drivers of hermeticity. Gross mass alone did not predict leak behaviour.
- PET-CF is a promising candidate for vacuum-retentive façade components when printed with appropriate parameters, but requires durability validation (environmental ageing, mechanical stress).
- PETG and PLA-Aero require process control improvements and/or post-processing (coatings, welding, annealing, adhesives) before deployment in hermetic applications.
- Standard PLA may be suitable where slow leakage is acceptable or where secondary sealing is applied; otherwise it is inferior to PET-CF for vacuum retention.
- Adopt routine pressure-decay acceptance testing for production batches, including blank-run baselines and leaky-reference controls.
- Define application-specific acceptance limits (e.g., maximum allowable decay at 60 min) linked to the functional requirements of the façade element (thermal performance, sensor reliability).
- Instrument detection limit (gauge ±0.05 bar) and 20-min initial sampling constrain sensitivity and temporal resolution; rapid leak events are reported as minimum bounds.
- Results are conditional on the tested geometry, single primary slicer profile, and laboratory environmental conditions. Different geometries, print orientations, filament batches, or post-processing protocols may yield different hermetic outcomes.
- Use higher-sensitivity methods (continuous pressure logging, helium mass spectrometry) to quantify small or fast leaks and convert decay to standardized leak-rate units.
- Conduct factorial parametric studies of print settings (temperature, flow, layer height, wall counts, orientation) for each material to identify optimal hermetic profiles.
- Evaluate post-processing treatments (coatings, annealing, welding) for efficacy and long-term retention under accelerated ageing (UV, moisture, thermal cycling).
- Scale testing to façade-representative geometries and multi-part assemblies; include mechanical loading and outdoor exposure trials.
- Develop application-specific acceptance criteria and contribute to standardization efforts for additively manufactured hermetic components in architecture.
Supplementary Materials
Author Contributions
Funding
Institutional Review Board Statement
Informed Consent Statement
Data Availability Statement
Acknowledgments
Conflicts of Interest
Abbreviations
| ASTM | American Society for Testing and Materials |
| BS EN | British Standards — European Norm |
| FDM | Fused Deposition Modeling |
| RH | Relative Humidity |
| NDE | Non-Destructive Evaluation |
| QC | Quality Control |
| PV | Pressure-Vacuum |
| PETG | Polyethylene Terephthalate Glycol |
| PET-CF | Carbon-fiber reinforced PET |
| PLA | Polylactic Acid |
| FFF | Fused Filament Fabrication |
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| Category | Details |
|---|---|
| Key concerns | - System performance compromise |
| - Risk of catastrophic failure - Long-term structural integrity issues |
|
| Applications | - Electronics: Prevents corrosion and short circuits - Biomedical Devices: Maintains sterility and prevents contamination - Aerospace/Automotive: Withstands extreme conditions and prevents failures - Energy Systems: Essential for containment and safety |
| Challenges | - Anisotropic properties [21] and internal voids - Micro-porosity and imperfect layer adhesion - Difficulties in traditional inspection methods |
| Conclusion | - Need for holistic design approaches - Emphasis on process control and advanced evaluation techniques |
| Method / Study | Context / Focus | Key finding / Relevance |
|---|---|---|
| Vacuum leak detection | General principle for hermetic sealing | High sensitivity, detects micro-leaks by exploiting gas migration under pressure differentials. |
| ASTM F2095 − 07 (Reapproved 2021) | Standardization for leak testing | Provides a comprehensive framework for repeatable and comparable leak testing, crucial for quality control in regulated industries. |
| Langlois, Hogreve, & Cappia (2017) | Validated pressure decay test for biopharmaceutical bags | Developed a robust, non-destructive pressure decay test (derived from ASTM F2095) capable of detecting 10 µm defects with high reliability, independent of bag volume. |
| Zaman et al. (2019) | Literature review on pipeline leak strategies | Comprehensive classification of hardware, software, and hybrid methods; highlights hybrid methods as most efficient for pressurized pipelines. |
| Ramadevi, Jaiganesh, & Krishnamoorthy (2018) | Review of pipeline leak detection technologies | Aims to identify adaptable, flexible, cost-effective, and efficient methods for real-time monitoring with low false alarm rates. |
| Colombo, Lee, & Karney (2009) | Literature review on transient-based leak detection | Explores hydraulic principles and pressure waves; notes a persistent lack of extensive field validation for these methods. |
| Filament type | Strength and properties | |
|---|---|---|
| Bambu PET-CF | Excellent strength, heat resistance, and low moisture absorption. Tensile strength: 74 MPa (X-Y), 35 MPa (Z) Impact strength: 36 kJ/m² (X-Y, notched), 4.5 kJ/m² (Z) |
|
| Bambu PLA Basic | High toughness, strong z-layer adhesion, and biodegradable properties. Tensile strength: 35 MPa (X-Y), 31 MPa (Z) Impact strength: 26.6 kJ/m² (X-Y, notched), 13.8 kJ/m² (Z) |
|
| Bambu PLA Aero | Lightweight with low density. Tensile strength: 24 ± 2 MPa (X-Y), 18 ± 3 MPa (Z) Impact strength: 28.8 kJ/m² (X-Y, notched), 8.2 kJ/m² (Z), 3.1 ± 0.7 kJ/m² (Z) |
|
| ReFill PETG by FormFutura | Amorphous, ultra-transparent filament with excellent strength and thermal stability. Tensile Strength: 50 MPa (Yield, ASTM D638) Impact Strength: 7.2 kJ/m² (notched, ASTM D256) Flexural Strength: 70.6 MPa (ASTM D790) Elongation at Break: 120% (ASTM D638) Specific Gravity: 1.27 g/cc (ASTM D792) |
|
| Material name | Mass (g) | Wall section image |
|---|---|---|
| PLA Basic | 22,95 | ![]() |
| PLA Aero | 13,79 | ![]() |
| PETG Translucent | 23,71 | ![]() |
| PET-CF | 23,17 | ![]() |
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