Public printing recommendation

Siraya Tech Fiberheart Gray ABS GF Gray

MaterialID MAT0201

3DPIceland Labs
Generated with 3DPIceland Engineering Platform v70.0.4 DIRECT-IMPACT-METHODOLOGY - Izod and Charpy Methodology
2026-10-04 18:12:06

Guidance boundary: values below are shared base-material guidance resolved only through the canonical BaseMaterialId link. They are not manufacturer-, spool- or printer-specific validated settings. Missing fields remain Not recorded.

Overall
38/100

Engineering axes
7/8

Public rank
69 / 80

MSRP USD/kg
25.07

Engineering profile

Overall

38/100

Tensile

17/100

Impact

—

Izod

11/100

Charpy

12/100

Stiffness

78/100

Consistency

66/100

Layer adhesion

16/100

Recommended applications

Rigid brackets, fixtures and shape-stable prototypes
Cosmetic parts, concept models or low-load prototypes
Avoid high tensile load applications
Avoid high impact components

Measured strengths

Stiffness: 78/100. Stiffness is a relative advantage in this comparison group.

Limitations

Tensile: 17/100. Avoid using this as the primary choice for tensile-loaded parts.
Izod/Charpy impact family: 12/100. Validate impact or shock-loaded components against their application requirements.
Layer adhesion: 16/100. Z-axis performance should be treated with caution.

Engineering trade-offs

Good repeatability does not compensate for low tensile capability in load-bearing designs.
Stiffness is useful for shape stability, but impact tolerance is a separate limitation.
The report should be read as a suitability warning rather than a general-purpose recommendation.

Base-material printing guidance

Guidance	Minimum	Recommended	Maximum	Unit
Nozzle temperature	250	255	265	°C
Bed temperature	110	110	110	°C
Print speed	55	165	165	mm/s
Cooling	15	20	20	%

Guidance	Value	Unit
Cooling guidance	Low
Drying temperature	75	°C
Drying time	6	hours
Enclosure	Required
Printer / G-code reference	PrusaCoreOneL
Slicer profile reference	Prusa Buddy3D ABS

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.
Reinforced filament: confirm an abrasion-resistant nozzle and manufacturer drying/storage requirements.
Engineering/high-temperature family: confirm enclosure, ventilation, warping control and material-specific drying requirements.
Layer-adhesion evidence is weak; avoid critical Z-axis loading without additional validation.

Decision guidance

Use this material mainly for low-load, visual or experimental parts.
Review the listed alternatives if the application needs stronger overall performance.
Do not choose it as a tensile-strength benchmark material.
Validate impact-focused or shock-loaded designs against the measured Izod/Charpy results.

Stronger same-family alternatives

MaterialID	Material	Manufacturer	Overall	Tensile	Impact	Izod	Charpy
MAT0246	Bedrock 3D Standard Black ABS Plus Black	Bedrock 3D	46/100	14/100	—	n/a	n/a
MAT0207	Siraya Tech Fiberheart Black ABS Core CF Black	Siraya Tech	46/100	24/100	—	n/a	n/a
MAT0199	Siraya Tech Fiberheart Black ABS CF Black	Siraya Tech	41/100	22/100	—	n/a	n/a

Confirm exact settings against the manufacturer profile, spool label and actual printer/material combination. Results do not replace application-specific validation.

Testing methodology · Download PDF

Izod and Charpy Impact Strength

Izod Impact Strength · 2026-09-30
Instrument readings in kJ/m²
Mean 8.994 kJ/m²; Std. Dev 1.61 kJ/m²; CV 17.896%; Samples 10; Confidence 10
No break 0; invalid 0; excluded 0.
Comparative measurements; standard conformity unverified.

Charpy Impact Strength · 2026-10-01
Instrument readings in kJ/m²
Mean 9.753 kJ/m²; Std. Dev 2.049 kJ/m²; CV 21.011%; Samples 9; Confidence 9
No break 0; invalid 0; excluded 0.
Comparative measurements; standard conformity unverified.

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.