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UMS40 UD-EP-60

Matrix

UD-EP-60 = uD epoxy laminate, 60 vol% UMS40

Pick for stiffness- and dimensional-stability-critical UD laminates (booms, optical benches, reflectors); compression and impact are the design limits.

High cost $$$$

Values for the UD-EP-60 condition

Other UMS40 grades and fills

UMS40 is listed in 4 conditions; see the grade overview at UMS40.

Compare all 4 grades and fillsHide
Grade · open for datasheetBest forYield MPaTensile MPaElong. %Hardness
Woven fabric epoxy laminate, ~55 vol% UMS40
Use where quasi-balanced, drapeable high-modulus skins are needed (panels, shells) at the cost of ~40 % lower 0° stiffness than UD.—850——
UD-EP-60This page
UD epoxy laminate, 60 vol% UMS40
Pick for stiffness- and dimensional-stability-critical UD laminates (booms, optical benches, reflectors); compression and impact are the design limits.—2,4001105 HRM
epoxy-compatible sizing, 24 000 filament tow (≈800 tex)
Heavier, lower-cost tow for thick wound or pultruded stiffness-driven sections and coarse UD tapes.—4,5001.2—
F22-12KDefault
epoxy-compatible sizing, 12 000 filament tow (≈400 tex)
Standard supply form for prepreg, filament winding and pultrusion with epoxy/BMI matrices.—4,5601.2—

What is UMS40 UD-EP-60?

UMS40 UD-EP-60 is UMS40 in the UD-EP-60 condition — pick for stiffness- and dimensional-stability-critical UD laminates (booms, optical benches, reflectors); compression and impact are the design limits. UMS40 UD-EP-60 has a tensile strength of 2,400 MPa (348 ksi), stronger than 78% of composite grades. Elongation at break is 1% and the elastic modulus is 240 GPa (34.8 Msi). UMS40 UD-EP-60 has a density of 1.6 g/cm³ (0.0578 lb/in³), lighter than 53% of composite grades. F22-12K is the default condition FabDigit quotes; UD-EP-60 is available on request or by drawing note.

Advantages

  • Stiff — 240 GPa (34.8 Msi), better than 85% of composite grades
  • Good corrosion resistance — 90/100, better than 85% of composite grades
  • Conducts heat well — 35 W/m·K (20.2 BTU/hr·ft·°F), better than 82% of composite grades
  • Good UV / weathering resistance — 95/100, better than 78% of composite grades

Limitations

  • High embodied carbon — 50 kg CO₂/kg, worse than 93% of composite grades
  • Limited ductility — 1%, worse than 80% of composite grades

UMS40 UD-EP-60 properties

Typical room-temperature values for UMS40 UD-EP-60; 19 are specific to this condition. Other listed values are UMS40 reference data and may not represent this condition. Bars are the position among composite grades.

Physical1

UMS40 UD-EP-60 has a density of 1.6 g/cm³ (0.0578 lb/in³), lighter than 53% of composite grades.

Density1.6 g/cm³0.06 lb/in³

Mechanical8

UMS40 UD-EP-60 has a tensile strength of 2,400 MPa (348 ksi), stronger than 78% of composite grades. Elongation at break is 1% and the elastic modulus is 240 GPa (34.8 Msi).

Elastic (Young's) Modulus240 GPa34.8 Msi
Poisson's Ratio0.3
Tensile Strength (Ultimate)2,400 MPa348 ksi
Elongation at Break1%
Compressive Strength900 MPa131 ksi
Flexural Strength1,300 MPa189 ksi
Flexural Modulus220 GPa31.9 Msi
Shear Strength85 MPa12.3 ksi

Thermal5

UMS40 UD-EP-60 is rated for continuous service to 150°C (302 °F). It conducts heat at 35 W/m·K (20.2 BTU/hr·ft·°F), better than 82% of composite grades. Thermal expansion is -0.9 µm/m·K (-0.5 µin/in·°F).

Thermal Conductivity35 W/m·K20.2 BTU/hr·ft·°F
Specific Heat Capacity710 J/kg·K0.17 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)-0.9 µm/m·K-0.5 µin/in·°F
Max Service Temperature (continuous)150°C302 °F
Min Service Temperature-269°C-452 °F

Electrical1

UMS40 UD-EP-60 has an electrical resistivity of 2×10⁻⁵ Ω·m.

Electrical Resistivity2×10⁻⁵ Ω·m787 µΩ·in

Chemical & Environmental3

Corrosion resistance is excellent (90/100), better than 85% of composite grades. UV resistance is excellent.

Corrosion ResistanceExcellent90/100
UV / Weathering ResistanceExcellent95/100
Chemical Resistance SummaryFiber itself is inert to most acids, alkalis, solvents and fuels; attacked only by hot strong oxidizers (conc. HNO3, chromic acid) and oxidizes in air above ~400 °C. In service the epoxy/BMI matrix and the fiber–matrix interface, not the fiber, set the chemical and moisture limits.

Sustainability4

Producing a kilogram of UMS40 UD-EP-60 takes about 700 MJ of energy and emits 50 kg of CO₂ — more than 90% of composite grades. Typical recycled content is 0%.

Embodied Energy (primary production)700 MJ/kg300,946 BTU/lb
Embodied Carbon (primary production)50 kg CO₂/kg
Embodied Water600 L/kg71.9 gal/lb
Typical Recycled Content0%

Manufacturability2

UMS40 UD-EP-60's machinability is poor (25/100, worse than 65% of composite grades).

MachinabilityPoor25/100
PolishabilityFair40/100

Values are nominal handbook figures for design screening. Confirm any required mill or lot documentation when quoting.

Working with UMS40 UD-EP-60

Is UMS40 easy to machine?

Cured laminates cut with PCD/diamond-coated or diamond-grit tooling at high speed and low feed; use up-cut/down-cut compression routers and backing to avoid delamination, and capture the conductive dust.

Can UMS40 be welded?

Not weldable — joints are made by co-curing, structural film/paste adhesive bonding or bolted metallic fittings (isolate from Al/steel with glass ply to avoid galvanic corrosion).

Can UMS40 be formed, bent or molded?

Processed as UD/woven prepreg (autoclave 120–180 °C cure), filament winding, AFP or RTM; the low strain-to-failure and high modulus mean generous fibre radii, careful tow tension and low-friction tooling paths.

What surface finishes work on UMS40?

Peel-ply or resin-rich surface plies then sand/fill/prime; UV-resistant topcoat or paint is required since the epoxy matrix chalks, and edges should be sealed against moisture ingress.

UMS40 chemical composition (wt %)

Limits by weight percent from the governing specification, written the way the spec states them — a single maximum for impurities, a range for alloying elements, and the base element as balance. Nominal is the typical mid-range value.

ElementSpec limit (wt %)Nominal
nitrogen (N)residual from PAN precursor≤ 10.4
epoxy-compatible sizing (F22)surface size, wt% of fiber0.7 – 1.51
carbon (C)graphitized PAN-based fiber≥ 98 (balance)—

UMS40 UD-EP-60 — frequently asked

What is UMS40 UD-EP-60 used for?

UMS40 UD-EP-60 is typically used for aircraft stiffness-critical parts, satellite structures and high-performance sports equipment. In short: 395 GPa PAN fiber; stiffness-critical aerospace laminates; low strain to failure.

What is the tensile strength of UMS40 UD-EP-60?

UMS40 UD-EP-60 has a typical tensile strength of 2,400 MPa (348 ksi) — stronger than 78% of composite grades. Strength varies by condition: see the 4 listed tempers.

Is UMS40 UD-EP-60 easy to machine?

Not especially — machinability is rated poor (25/100, worse than 65% of composite grades). Cured laminates cut with PCD/diamond-coated or diamond-grit tooling at high speed and low feed; use up-cut/down-cut compression routers and backing to avoid delamination, and capture the conductive dust.

Can UMS40 UD-EP-60 be welded?

Not weldable — joints are made by co-curing, structural film/paste adhesive bonding or bolted metallic fittings (isolate from Al/steel with glass ply to avoid galvanic corrosion).

What surface finishes work on UMS40 UD-EP-60?

Peel-ply or resin-rich surface plies then sand/fill/prime; UV-resistant topcoat or paint is required since the epoxy matrix chalks, and edges should be sealed against moisture ingress.

Can UMS40 UD-EP-60 be formed, bent or molded?

Processed as UD/woven prepreg (autoclave 120–180 °C cure), filament winding, AFP or RTM; the low strain-to-failure and high modulus mean generous fibre radii, careful tow tension and low-friction tooling paths.

What is the maximum service temperature of UMS40 UD-EP-60?

UMS40 UD-EP-60 is rated for continuous use to about 150°C (302 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

Sources

  1. Tenax filament yarn product data sheet (UMS40 F22) — Teijin Carbon Europe GmbH (2023)
  2. ISO 11566 — Carbon fibre: determination of tensile properties of single-filament specimens — ISO (1996)
  3. ISO 10618 — Carbon fibre: determination of tensile properties of resin-impregnated yarn — ISO (2004)
  4. ASM Handbook Vol. 21: Composites — ASM International (2001)
  5. MMPDS / CMH-17 typical carbon/epoxy lamina data — CMH-17 / Battelle (2019)

Property data is compiled from published supplier and standards handbooks and normalised for comparison. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.