Composite KPIs
Composite Manufacturing KPIs and Benchmarks: The Numbers That Matter
The KPIs that matter in composite and fiberglass production, from first-pass yield and nesting yield to autoclave loading, scrap and fiber volume: how to measure each, what moves it, and which figures have a cited source.
Composite and fiberglass production turns on a handful of KPIs: first-pass yield, material utilization, cure asset utilization, scrap, labor productivity and laminate quality. Use the ranges below as reference points for spotting a gap worth investigating, not as targets.
Every figure shows its basis. A superscript number links to a public source in the Sources list, and the sentence states what that source covers. A figure marked no cited source is kept exactly as originally published because no public source stating it has been found, so treat it as illustrative.
At a glance
| KPI | Typical | Strong | Basis |
|---|---|---|---|
| First-pass yield, stable parts | 80 to 90% | 95% or better (world-class prepreg lines) | no cited source |
| First-pass yield, new-program launch | Near 60 to 70% (often starts) | Not stated | no cited source |
| Material waste, hand nesting on complex parts | 25 to 40% | Not stated | no cited source |
| Material utilization | Not stated | 80 to 88% (automated ply nesting); > 90% (world-class flat-pattern work) | no cited source |
| Autoclave utilization | 45 to 60% (many shops) | 75 to 85% (world-class scheduling) | no cited source |
| Prepreg molding cycle time | 5 to 10 hours | Not stated | U.S. DOE1 |
| Scrap, fiber-reinforced composite manufacturing | 15 to 25% | Not stated | U.S. DOE2 |
| Prepreg scrap, share of purchased material | Not stated | < 12% (disciplined shops); near 8% (world class) | no cited source |
| Hand layup rate, woven fabric | 40 to 70 ply-sq ft per hour | Not stated | no cited source |
| Fiber volume fraction, autoclave prepreg | 55 to 60% | Not stated | Hexcel3 |
| Fiber volume fraction, wet layup | 35 to 45% (target band) | Not stated | no cited source |
| Void content | Not stated | < 2% (structural aerospace limit); < 1% (most critical parts) | no cited source |
Method: How the figures in this guide are sourced
A figure with a superscript number is stated by the cited source, listed under Sources with its publisher, location in the document and access date. The cited figures come from a U.S. Department of Energy technology assessment and a prepreg maker's technical guide, and the text gives their scope. A figure marked no cited source is kept exactly as originally published because no public source stating it has been found. It is illustrative, not measured industry data. Worked examples are arithmetic, not benchmarks.
First-pass yield
First-pass yield (FPY) is the headline composite KPI because rework is slow and often impossible. Typical shops run 80 to 90 percent FPY on stable parts no cited source; world-class prepreg lines hold 95 percent or better no cited source.
New-program launches often start near 60 to 70 percent no cited source. Set the control-plan target at the world-class level and track the gap as the program matures.
How to measure
- Divide parts accepted without repair by parts produced.
- Keep the part family and the period the same for both counts.
- Report new-program parts separately from stable ones.
What moves it
- Ply orientation poka-yoke, since misoriented plies drive many first-pass failures.
- Operator certification.
- Tool condition, since worn molds are the other common cause.
Material utilization
Material utilization, or nesting yield, is the second big lever because fiber is the largest cost line. Hand nesting on complex parts wastes 25 to 40 percent no cited source. Automated ply nesting pushes utilization to 80 to 88 percent, and world-class flat-pattern work exceeds 90 percent no cited source.
Every point of yield recovered on a shop buying 68 dollar per lb prepreg is real cash no cited source.
How to measure
- Divide usable ply area by consumed roll area.
- Report it per material and per part family.
What moves it
- Automated nesting software.
- Common blanks shared across part numbers.
- Tighter kit cut plans, so trim strips get reused rather than scrapped.
Put a price on each point of yield with the Carbon Fiber Material Cost calculator.
Autoclave and cure asset utilization
Autoclave and cure asset utilization decides how much of your fixed cost earns money. Many shops run autoclaves at 45 to 60 percent utilization with half-empty loads no cited source; world-class scheduling reaches 75 to 85 percent by batching parts with matching cure cycles no cited source.
Long cycles make batching matter. The U.S. Department of Energy's 2015 Quadrennial Technology Review lists a cycle time of 5 to 10 hours for prepreg molding1, which is why loads should be batched by cure cycle.
How to measure
- Divide charged cure hours by available hours for utilization.
- Divide parts per load by rated capacity for loading efficiency.
- Test whether the schedule fits cure capacity before committing dates.
What moves it
- Cure-cycle families that let parts share a load.
- Load planning that fills the envelope.
- Moving low-temperature parts to ovens, so the autoclave runs only what needs pressure.
Cost a cure load with the Autoclave Cycle Cost calculator.
Scrap rate
Scrap rate deserves its own KPI, split into prepreg scrap and cured trim scrap. Across fiber-reinforced composite manufacturing as a whole, the U.S. Department of Energy's 2015 Quadrennial Technology Review puts scrap at 15 to 25 percent2.
For prepreg scrap as a percent of purchased material, disciplined shops hold it under 12 percent, and world class stays near 8 percent no cited source. Cured trim scrap is harder to recover, since the labor and cure are already spent.
Freezer-expiry scrap should be near zero with proper out-time tracking. Prepregs typically carry a guaranteed shelf life of 12 months at minus 18 degrees Celsius from the date of manufacture, according to Hexcel4, so expired stock is a rotation failure.
How to measure
- Report prepreg scrap as a percent of purchased material.
- Report cured trim scrap separately.
- Log freezer-expiry scrap as its own line.
What moves it
- Out-time and shelf-life monitoring.
- Net-shape ply cutting.
- Precise CNC-driven kits in place of oversize blanks.
Price the material you scrap with the Carbon Fiber Material Cost calculator.
Labor productivity
Labor productivity is measured in ply-square-feet placed per labor hour, and it exposes staffing and training gaps. Hand layup of woven fabric runs 40 to 70 ply-sq ft per hour no cited source.
Automated fiber placement reaches thousands of times that on large surfaces but only justifies itself at volume no cited source.
How to measure
- Divide ply-square-feet placed by labor hours on the tool.
- Benchmark crews against a time-studied rate for the same fabric and complexity, not a shop average.
What moves it
- Standardized work.
- Kitting, so laminators never leave the tool to hunt for material.
- Debulk scheduling that removes idle waiting from the placement clock.
Estimate layup hours for a part with the Composite Layup Labor calculator.
Laminate quality
Laminate quality holds to tight physical targets that double as process KPIs. Fiber volume fraction should land at 55 to 60 percent for autoclave prepreg3 and 35 to 45 percent for wet layup no cited source.
Hexcel's typical property tables for epoxy prepreg laminates give a fiber volume of about 60 percent for carbon and about 50 percent for E-glass and aramid3. The band above therefore fits carbon prepreg best.
Void content must stay under 2 percent for structural aerospace parts and under 1 percent for the most critical no cited source. Cured ply thickness should track the ply book within a few thousandths of an inch no cited source.
How to measure
- Measure fiber volume and void content on witness panels or coupons from the same cure.
- Compare cured ply thickness with the ply book value.
- Treat drift outside the bands as a sign of compaction, vacuum or cure problems.
What moves it
- Vacuum integrity checks.
- Correct debulk frequency.
- Validated cure profiles with thermocouple coverage across the load.
Cost the bagging that holds vacuum with the Vacuum Bagging Cost calculator. For wet layup and infusion, check resin quantity with the Fiberglass Resin Usage calculator and fill time with the Resin Infusion Time calculator.
On-time delivery and cycle metrics
On-time and cycle metrics tie the technical KPIs to delivery. Track cure asset lead time, layup-to-cure queue time and schedule adherence.
A shop holding 95 percent FPY, 85 percent material utilization, 80 percent autoclave utilization and under 12 percent scrap will usually also hit 95 percent on-time no cited source, because the same discipline that controls quality controls flow.
Improve the KPIs in order. Stabilize FPY first so you stop rebuilding scrapped parts, then chase utilization and scrap, since chasing throughput on an unstable process just produces defects faster and buries the gains you thought you booked.
How to build your own baseline
- Write each KPI's definition down and keep it fixed.
- Measure per part family, per material and per cure asset before averaging.
- Compare against your own trend first and published ranges second.
- Record what changed in the process whenever a KPI moves.
Sources
- Quadrennial Technology Review 2015, Technology Assessment 6.E: Composite Materials. U.S. Department of Energy. published 2015. p. 19 (PDF p. 20), Table 6.E.4 'Comparison of the Most Commonly Used Composite Molding Processes', Pre-preg row. Accessed September 30, 2026.
- Quadrennial Technology Review 2015, Technology Assessment 6.E: Composite Materials. U.S. Department of Energy. published 2015. p. 27 (PDF p. 28), recycling discussion, sentence citing ref. 118 (Gosau et al., SAMPE 2001). Accessed September 30, 2026.
- Prepreg Technology (Publication No. FGU 017c). Hexcel Corporation. published January 2013. pp. 27-28, tables 'Typical mechanical values on epoxy prepreg laminates' and 'Typical thermal properties of prepreg laminates'. Accessed September 30, 2026.
- Prepreg Technology (Publication No. FGU 017c). Hexcel Corporation. published January 2013. p. 29, 'Storage' section. Accessed September 30, 2026.
Published 2026-07-01.