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newSchoolWorks.com › VoTechWorks › Manufacturing & Marine › Fiberglass / Composites (boatbuilding) › Mold Making for Fiberglass and Composite Boatbuilding › Lesson 6
MFG-COMP18-02 · Lesson 6 · 14 clock hours · lab

Build-Up Laminate, Flanges, and Stiffener Integration

Objective. Students will complete a mold laminate schedule by applying build-up plies and perimeter flanges to achieve a minimum cured laminate thickness specified on the schedule, and bond or integrate stiffening structure.

⚠ Pending professional review

This lesson, its worked examples and its practice questions has not yet been verified by a licensed engineer or certified journey-level tradesperson or by a certification or approval body. It is a study draft and may contain errors. Do not use it as instructions for work on a job site or on live equipment. Always follow your instructor, your supervising professional, and current official references and regulations.

VoTechWorks program approval and accreditation are still in progress. Credentials are issued only by the certifying bodies named in each program, after their own exams.

Why Build-Up Laminate Matters in Mold Making

A production mold must survive hundreds of part pulls without warping, cracking, or losing its surface geometry. The skin coat you applied in earlier sessions captures the surface finish; the build-up laminate gives the mold its structural depth, stiffness, and thermal mass. Skipping plies or rushing cure cycles between layers are the two most common reasons molds fail early in a production run. Following your tooling laminate schedule exactly—ply by ply, with correct resin-to-reinforcement ratios—is the professional standard.

Reading and Following a Tooling Laminate Schedule

Your instructor-issued schedule will list each ply in order, the fabric type, weight, and the target resin-to-reinforcement ratio for that ply. A typical demonstration-mold schedule looks like this:

1. Skin coat (tooling gelcoat, already applied)

2. Barrier ply — 1.5 oz chopped-strand mat (CSM), ratio ≈ 2:1 resin to glass by weight

3. Second ply — 1.5 oz CSM, ratio ≈ 2:1

4. Third ply — 1.5 oz CSM, ratio ≈ 2:1

5. Fourth ply — 24 oz woven roving (WR), ratio ≈ 1.5:1

6. Fifth ply — 24 oz woven roving (WR), ratio ≈ 1.5:1

CSM uses more resin than woven roving because the random-chopped fibers have more void space to fill. Woven roving is denser, so less resin is needed per ounce of fabric. Recording the actual ratio you achieve in your lab log lets you trace problems (voids, resin-rich areas) back to a specific ply.

Mixing Resin and Catalyst Accurately

Tooling resins are catalyzed with methyl ethyl ketone peroxide (MEKP). The manufacturer's technical data sheet (TDS) specifies the acceptable MEKP percentage range—typically between 1 % and 2 % by weight of the resin. Working outside that range causes incomplete cure or dangerously fast exotherm. Always weigh resin and catalyst on a gram scale; do not estimate by eye or use volumetric cups for catalyst.

Pot life at your shop temperature will be printed on the TDS. Mix only what you can apply in roughly two-thirds of the stated pot life to avoid catalyzing a batch that gels in the container. Discard any batch that begins to warm noticeably in the cup—it is gelling and must not be applied.

Wetting Out Fabric and Consolidating Plies

Pour resin onto the fabric, not fabric onto a pool of resin. Work the resin in from the center outward with a brush, then pass a segmented steel roller firmly across the surface in overlapping strokes. The roller breaks up air pockets trapped under and between fibers. A properly wetted-out ply looks translucent; white or milky areas indicate trapped air and must be re-rolled before the next ply goes down. Resin-starved areas appear dull and fibrous—add resin and re-roll immediately.

Allow each CSM ply to reach a gel state (firm to the touch, not tacky) before applying the next, unless your schedule specifies a wet-on-wet stack. Woven roving can create print-through telegraph lines in the mold surface if laid too close to the skin coat; the CSM barrier plies prevent this.

Building Perimeter Flanges

A flange is an extension of the mold laminate that runs around the entire perimeter of the part boundary. Flanges serve three purposes: they provide a clamping surface when bolting mold halves together, a reference datum for locating the parting plane, and a structural lip that resists edge warping. Industry practice requires flanges to extend at least 2 inches beyond the part boundary.

Cut your flange fabric from the same schedule as the body plies. Lap the flange plies onto the mold body by at least 2 inches so the flange is structurally continuous with the mold shell. After cure, check flange thickness with calipers at all four corners; all readings must meet the schedule minimum.

Secondary Bonding of Stiffeners

After the mold laminate is fully cured, stiffening structure—hat-section extrusions, square tubing, or plywood risers—is bonded to the back of the mold. This is a secondary bond: the bond relies on adhesion to a cured surface rather than co-cure. Prepare the bonding surface by sanding with 80-grit paper and wiping with an appropriate solvent, following the resin manufacturer's guidance. A poorly prepared surface is the leading cause of stiffener delamination in service.

Set stiffeners parallel to each other and square to the mold edge using a framing square. Bond with wet laminate (strips of CSM wetted with catalyzed resin tabbed over each stiffener edge) or with a structural methacrylate or epoxy adhesive as your instructor specifies. Let the completed assembly cure fully before handling.

Measuring and Accepting the Finished Mold Back

After cure, use a 0–6 inch caliper to measure laminate thickness at six representative points across the panel and at each flange corner. Every reading must meet or exceed the schedule minimum—typically 3/8 inch (approximately 9.5 mm) for a demonstration mold of this size. Any point below minimum requires an additional ply bonded over that area before the mold receives sign-off. Document all readings in your lab log with a dimensioned sketch showing measurement locations.

Safety Requirements for This Lab

Tooling resins and MEKP are serious chemical hazards. MEKP is a strong oxidizer that can cause severe eye and skin burns on contact; store it away from all organic materials and never mix it in a sealed container. Wear a full-face respirator fitted with organic-vapor/P100 combination cartridges—safety glasses alone are not adequate protection from styrene vapor or resin mist. Nitrile gloves (minimum 8-mil thickness) and a Tyvek coverall protect skin from prolonged resin contact, which can cause sensitization. Work with local exhaust ventilation running. Follow your shop's lockout/tagout procedures before using any powered mixing or grinding equipment. Dispose of resin-soaked materials in a metal container with a lid; curing exotherms in waste bins can cause fires.

Key terms10

Tooling laminate scheduleA written ply-by-ply list specifying fabric type, weight, sequence, and target resin-to-reinforcement ratio used to build a mold to its required thickness and stiffness.
Chopped-strand mat (CSM)A non-woven fiberglass reinforcement made of randomly oriented short glass fibers held together with a binder; used in mold build-up for its conformability and ability to block print-through.
Woven rovingA heavy fiberglass fabric woven from continuous rovings; used in mold laminates to add structural thickness and stiffness efficiently.
Resin-to-reinforcement ratioThe weight of wet resin applied divided by the weight of dry fiber reinforcement; a key quality metric for each ply recorded in the lab log.
Segmented consolidation rollerA steel roller with independently moving discs that conforms to curved surfaces, used to work air bubbles out of wet laminates and ensure full fiber wet-out.
FlangeA flat extension of the mold laminate extending at least 2 inches beyond the part boundary; provides a parting surface, clamping area, and edge stiffness.
Secondary bondA bond made to a fully cured laminate surface, relying on adhesion rather than co-cure; used to attach stiffeners to the mold back after the mold shell has cured.
MEKP (methyl ethyl ketone peroxide)The organic peroxide catalyst used to initiate cure in polyester and vinyl ester tooling resins; a strong oxidizer requiring careful handling and precise measurement by weight.
ExothermThe heat generated by the chemical crosslinking reaction as resin cures; excessive exotherm from over-catalysis or thick batch volumes can cause cracking, distortion, or fire.
Print-throughSurface distortion on the mold face caused by the coarse texture of woven roving telegraphing through inadequate barrier plies; prevented by applying CSM barrier layers between the gelcoat and structural fabric.

Worked examples4

1. You are applying a ply of 1.5 oz CSM. The dry fabric weighs 210 grams. The target resin-to-reinforcement ratio is 2:1 by weight. How many grams of catalyzed resin should you mix for this ply?
  1. Identify the ratio: 2 parts resin to 1 part reinforcement by weight.
  2. Multiply the dry fabric weight by the ratio: 210 g × 2 = 420 g of resin needed.
  3. Mix 420 grams of catalyzed resin for this ply.
Answer: 420 grams of catalyzed resin.
2. Your tooling resin TDS calls for 1.5 % MEKP by weight. You weigh out 350 grams of resin. How many grams of MEKP must you add?
  1. Convert the percentage to a decimal: 1.5 % = 0.015.
  2. Multiply resin weight by the decimal: 350 g × 0.015 = 5.25 g.
  3. Add 5.25 grams of MEKP to the resin and mix thoroughly.
Answer: 5.25 grams of MEKP.
3. After cure you measure laminate thickness at six points with calipers: 0.390 in, 0.405 in, 0.372 in, 0.381 in, 0.410 in, and 0.355 in. The schedule minimum is 0.375 in (3/8 in). Which points are non-conforming and what action is required?
  1. List the minimum: 0.375 inch.
  2. Compare each reading to the minimum: 0.390 — pass; 0.405 — pass; 0.372 — FAIL (0.003 in below minimum); 0.381 — pass; 0.410 — pass; 0.355 — FAIL (0.020 in below minimum).
  3. Identify the two non-conforming points: the third reading (0.372 in) and the sixth reading (0.355 in).
  4. Required action: sand the area lightly to prepare the surface, apply at least one additional ply of the specified fabric over each non-conforming zone, allow to cure, then re-measure before sign-off.
Answer: Two points are non-conforming (0.372 in and 0.355 in); an additional ply must be applied over each deficient area and re-measured before the mold can be accepted.
4. Your flange must extend at least 2 inches beyond the part boundary on all four sides. You are cutting flange strips from a panel that is 18 inches wide. The part boundary runs 14 inches across the panel width. How wide must each flange strip be if the strip also needs to lap 2 inches onto the mold body?
  1. The flange must reach at least 2 inches beyond the part boundary on the outside.
  2. The flange strip must also overlap 2 inches onto the mold body on the inside.
  3. Total strip width needed = 2 in (body lap) + 2 in (extension beyond part boundary) = 4 inches minimum.
  4. Cut flange strips at least 4 inches wide.
Answer: Each flange strip must be at least 4 inches wide.

The math in this lesson3

Learners apply a 2:1 resin-to-reinforcement ratio to find resin grams for a CSM ply.
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Brush up in the math halls at newSchoolWorks.com:
In class: Students follow an instructor-provided tooling laminate schedule (e.g., skin coat + 3 layers 1.5 oz CSM + 2 layers woven roving at 24 oz) to build laminate thickness on their mold panels, mixing resin and catalyst for each batch on a gram scale, wetting out fabric, and rolling out air with a segmented consolidation roller; they record resin-to-reinforcement ratio for each ply in the lab log. · Students cut and lay flanges around the perimeter of the mold panel using the same laminate schedule, extending at least 2 inches beyond the part boundary to provide a clamping and parting surface; flanges are checked for uniform thickness with calipers at four corners. · After cure, students bond 1-inch square tubular fiberglass or plywood hat-section stiffeners to the mold back using a secondary bond (wet-laminate or adhesive as specified), ensuring stiffeners are parallel and square with a framing square; the completed mold back is photographed and logged.
Materials: Tooling laminate schedule (instructor-issued), 1.5 oz chopped-strand mat, 24 oz woven roving, tooling resin, MEKP, gram scale, segmented steel roller, mixing containers, calipers (0–6 inch), framing square, fiberglass or plywood stiffener stock, secondary bond adhesive or wet-laminate materials, scissors, marking pen, lab log, PPE (full-face respirator OV/P100, nitrile gloves, Tyvek, safety glasses)
Check: Cured laminate thickness is measured with calipers at six points; all readings must meet or exceed the scheduled minimum (typically 3/8 inch for a demonstration mold of this size); flange width is verified at 2 inches minimum at all four corners; any point below minimum requires an additional ply before sign-off.

Practice check8

Answer each question, then check it. Nothing is recorded; this is your own practice.

Mold construction and tooling
1. Which primary purpose do perimeter flanges serve on a fiberglass production mold?
Reinforcement materials and laminate design
2. Why is chopped-strand mat (CSM) used as a barrier ply between the tooling gelcoat and woven roving in a mold laminate?
Resin systems and processing
3. A technician weighs 280 grams of resin and must add MEKP at 1.5 % by weight. How many grams of MEKP are required?
Quality control and inspection
4. When measuring cured laminate thickness for mold acceptance, a reading of 0.360 inches is found at one location where the schedule minimum is 0.375 inches. What is the correct corrective action?
Health, safety, and hazardous materials
5. What is the primary hazard of allowing a resin-and-catalyst batch to begin warming noticeably in the mixing cup?
Health, safety, and hazardous materials
6. Which respiratory protection is required when hand-laminating with styrene-containing tooling resin in a shop with local exhaust ventilation?
Bonding, joining, and assembly
7. A secondary bond is used to attach stiffeners to the mold back. What surface preparation is required before bonding to a fully cured laminate?
Reinforcement materials and laminate design
8. According to standard mold-building practice, the resin-to-reinforcement ratio for 1.5 oz CSM is approximately 2:1 by weight, while 24 oz woven roving typically requires approximately 1.5:1. Why does CSM require more resin per unit weight of fabric?
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