
ANSI
View official documentation (opens in new tab)ANSI Z136.1, Safe Use of Lasers[1]

Wax and silicone mold-release films on CFRP bond coupons block adhesive work until the crew picks UV or picosecond prep. Coupon passes near 1 J/cm² single-pulse clear thin resin when 1064 nm IR would heat carbon fiber first. Ground HEPA capture handles conductive dust under OSHA PNOR rows after the strip. (NASA picosecond CFRP 2017; Alphanov CFRP paint 2017)
Standard fiber IR gives no safe margin on thin carbon laminates because release wax and epoxy resin absorb together, the contaminant and the matrix ablate as one. Atmospheric plasma remains the shop-floor bonding standard while laser prep stays underdeveloped on production panels. Zhu's 2025 review puts published CFRP paint-strip throughput at 6–372 cm²/min against a 929 cm²/min industrial floor.
Laser prep can activate CFRP bond faces when wavelength and line spacing stay on labeled coupons, though residual silicone still kills lap-shear performance at trace levels. Picosecond NASA Langley work delivered about one joule per pulse single-shot with twenty-five joules per square centimeter total accumulated fluence on epoxy composite coupons, a labeled recipe, not a fleet default. Water-break checks still matter after the strip pass.
GFRP gel-coat jobs need wider coupon bands than CFRP mold release when the target is polyester gel coat, not carbon-filled laminate. NAVAIR diode-laser work removed pigmented gel coat without apparent fiber damage at tested power on fiberglass epoxy panels. Hold fluence on a gel-coat coupon before copying any carbon-composite default from the layup bay.
National laser-safety enclosure rules and plastics bonding surface practice apply to CFRP mold tooling and production ply stock alike before any pulsed head crosses the layup bay. (ANSI Z136.1; ASTM D2093)

ANSI Z136.1, Safe Use of Lasers[1]

ASTM D2093, Standard Practice for Preparation of Surfaces of Plastics Prior to Adhesive Bonding[2]
Atmospheric plasma remains the shop-floor standard for composite activation on production panels, while laser cleaning controls resin depth plasma cannot target. Published CFRP paint strip throughput on those same coupon panels runs 6–372 cm²/min against a ≥929 cm²/min Joint Test Protocol industrial floor in Zhu's 2025 review. (Zhu CFRP paint review 2025; MDPI plasma automotive 2024; Composite manufacturing applications; ANSI Z136.1 — Safe Use of Lasers; BAAQMD Regulation 6 — Particulate Matter, Common)
Abrasion / grit blasting
Peel ply + solvent wipe
Atmospheric plasma treatment
CFRP is the defining substrate for this contaminant family and the most dangerous laminate on labeled bond coupons. Organic contaminant and epoxy matrix absorb similarly at 1064 nm on carbon fiber composite. Fiberglass coupon panels accept higher fluence when gel coat limits stay tested.
| Substrate | Ablation threshold (J/cm²) | Substrate damage (J/cm²) | Process window | Regime |
|---|---|---|---|---|
| CFRP (release agent / surface contamination) | 0.3–1.5 | 1.5–3 | 1–10×Narrow — resin matrix ablates close to fiber damage; 1064 nm IR margin effectively zero on thin laminates | sublimation-ablation |
| GFRP (gel coat / surface contamination) | 0.5–2 | 2–5 | 1–10×Moderate — gel coat clears below glass/resin damage when fluence stays on coupon-tested bands | sublimation-ablation |
Release-agent chemistry, PDMS bond sensitivity, CFRP damage bands, gel-coat targets, and 1064 nm selectivity limits, each row drives a separate planning decision on labeled layup coupons.
| Parameter | Value |
|---|---|
| Release agent families | Wax, silicone, PVA film, fluoropolymer spray, semi-permanent solvent systems |
| Bond sensitivity to PDMS | Mode I fracture toughness drops ~50% at 1.7 µg/cm² PDMS residue |
| CFRP damage band (ns) | 4.1 J/cm² SP-UV to ~8.3 J/cm² IR picosecond |
| Selectivity problem at 1064 nm | Contaminant and epoxy matrix share organic absorption — no single-IR selectivity |
| Gel coat on fiberglass | Pigmented polyester/epoxy mold layer strips without fiber damage at tested diode power |
| Aerospace paint on CFRP | Multi-layer primer plus topcoat; femtosecond thresholds below 0.25 J/cm² on coupon work |
| Carbon fiber IR absorption | Epoxy damage 10.7 J/cm² SP-UV; CFRP composite damage begins near 4.1 J/cm² |
Working fluence ~0.45 J/cm² on CFRP (release agent / surface contamination) (representative substrate — see table above for others) (window 0.30–1.50 J/cm²). Bars: datasheet max pulse energy; color: process status.
Five main release agent categories: wax-based (carnauba, PTFE), silicone-based (polydimethylsiloxane/PDMS), semi-permanent (solvent-based polymer films), PVA (polyvinyl alcohol) water-soluble film, and FEP (fluorinated ethylene propylene) film. Different chemistry produces different laser absorption behavior and ablation thresholds (compositesworld-mold-release-systems).