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P100Gr/6061Al UD45-F

Reinforced grade · default condition

UD45-F = uD Vf≈45%

Standard unidirectional Vf≈45% plate in as-fabricated condition: near-zero axial expansion and 320 GPa modulus suit truss struts and other one-dimensional load paths, with only 0.3 % elongation.

High cost $$$$

Values for the UD45-F condition

Other P100Gr/6061Al grades and fills

P100Gr/6061Al is listed in 5 conditions; see the grade overview at P100Gr/6061Al.

Compare all 5 grades and fillsHide
Grade · open for datasheetBest forYield MPaTensile MPaElong. %Hardness
Quasi-isotropic [0/±45/90] laminate
Use for housings and mounting plates with multidirectional loads or isotropic dimensional stability; the [0/±45/90] lay-up gives the smallest stiffness gain (130 GPa) but the simplest design.2302500.4—
[0/90] cross-ply laminate
Choose for panels and baseplates loaded in two directions: the cross-plied lay-up balances stiffness (175 GPa) and CTE in both principal axes, with in-plane expansion tunable to near zero.—3300.3—
Solution heat treated and artificially aged
Use when matrix-dominated transverse, shear and bearing strength must be raised; the solution-treated and artificially aged matrix needs tight temperature and time control to avoid interfacial Al4C3 and residual thermal stress.5806600.25—
UD Vf≈55%
Pick for maximum axial stiffness (400 GPa), 380 W/m·K conduction and near-zero or negative CTE; at ~55% fibre volume the transverse and shear properties drop further.6007000.25—
UD45-FDefaultThis page
UD Vf≈45%
Standard unidirectional Vf≈45% plate in as-fabricated condition: near-zero axial expansion and 320 GPa modulus suit truss struts and other one-dimensional load paths, with only 0.3 % elongation.—6200.3—

What is P100Gr/6061Al UD45-F?

P100Gr/6061Al UD45-F is P100Gr/6061Al in the UD45-F grade — standard unidirectional Vf≈45% plate in as-fabricated condition: near-zero axial expansion and 320 GPa modulus suit truss struts and other one-dimensional load paths, with only 0.3 % elongation. P100Gr/6061Al UD45-F has a tensile strength of 620 MPa (89.9 ksi), stronger than 69% of composite grades. Elongation at break is 0.3% and the elastic modulus is 320 GPa (46.4 Msi). P100Gr/6061Al UD45-F has a density of 2.5 g/cm³ (0.0903 lb/in³), heavier than 81% of composite grades.

Advantages

  • Conducts heat well — 320 W/m·K (184.9 BTU/hr·ft·°F), better than 98% of composite grades
  • Stiff — 320 GPa (46.4 Msi), better than 93% of composite grades

Limitations

  • Needs corrosion protection — 28/100, worse than 99% of composite grades
  • Limited ductility — 0.3%, worse than 95% of composite grades
  • Difficult to machine — 12/100, worse than 89% of composite grades
  • High embodied carbon — 32 kg CO₂/kg, worse than 84% of composite grades
  • Heavy — 2.5 g/cm³ (0.0903 lb/in³), worse than 81% of composite grades

P100Gr/6061Al UD45-F properties

Typical room-temperature values for P100Gr/6061Al UD45-F; 12 are specific to this condition. Other listed values are P100Gr/6061Al reference data and may not represent this condition. Bars are the position among composite grades.

Physical1

P100Gr/6061Al UD45-F has a density of 2.5 g/cm³ (0.0903 lb/in³), heavier than 81% of composite grades.

Density2.5 g/cm³0.09 lb/in³

Mechanical11

P100Gr/6061Al UD45-F has a tensile strength of 620 MPa (89.9 ksi), stronger than 69% of composite grades. Elongation at break is 0.3% and the elastic modulus is 320 GPa (46.4 Msi).

Elastic (Young's) Modulus320 GPa46.4 Msi
Shear Modulus30 GPa4.4 Msi
Poisson's Ratio0.3
Tensile Strength (Ultimate)620 MPa89.9 ksi
Elongation at Break0.3%
Compressive Strength420 MPa60.9 ksi
Compressive Modulus310 GPa45 Msi
Flexural Strength550 MPa79.8 ksi
Flexural Modulus290 GPa42.1 Msi
Shear Strength50 MPa7.3 ksi
Fracture Toughness (K_IC)12 MPa·√m10.9 ksi·√in

Thermal6

P100Gr/6061Al UD45-F is rated for continuous service to 350°C (662 °F). It conducts heat at 320 W/m·K (184.9 BTU/hr·ft·°F), better than 98% of composite grades. Thermal expansion is 0.5 µm/m·K (0.278 µin/in·°F).

Thermal Conductivity320 W/m·K185 BTU/hr·ft·°F
Specific Heat Capacity820 J/kg·K0.2 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)0.5 µm/m·K0.28 µin/in·°F
Max Service Temperature (continuous)350°C662 °F
Min Service Temperature-269°C-452 °F
Max Service Temperature (short-term)450°C842 °F

Electrical1

P100Gr/6061Al UD45-F has an electrical resistivity of 5×10⁻⁸ Ω·m.

Electrical Resistivity5×10⁻⁸ Ω·m1.97 µΩ·in

Chemical & Environmental3

Corrosion resistance is poor (28/100), worse than 99% of composite grades. UV resistance is excellent.

Corrosion ResistancePoor28/100
UV / Weathering ResistanceExcellent92/100
Chemical Resistance Summary—

Sustainability3

Producing a kilogram of P100Gr/6061Al UD45-F takes about 480 MJ of energy and emits 32 kg of CO₂ — more than 81% of composite grades. Typical recycled content is 0%.

Embodied Energy (primary production)480 MJ/kg206,363 BTU/lb
Embodied Carbon (primary production)32 kg CO₂/kg
Typical Recycled Content0%

Manufacturability2

P100Gr/6061Al UD45-F's machinability is not recommended (12/100, worse than 89% of composite grades).

MachinabilityNot recommended12/100
PolishabilityFair35/100

Common Calculations4

Specific Strength (UTS / density)calculated248 kN·m/kg
Specific Stiffness (E / density)calculated128 MN·m/kg
Thermal Diffusivitycalculated156.1 mm²/s
Thermal Shock Resistance Indexcalculated1,240

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

Working with P100Gr/6061Al UD45-F

Is P100Gr/6061Al easy to machine?

Requires PCD or CVD-diamond tooling at high speed and low feed with full coolant to avoid fiber pull-out and delamination. Use water-guided laser or diamond grinding for holes and edge trimming; ordinary carbide tool life is extremely short.

Can P100Gr/6061Al be welded?

Not fusion weldable — the weld pool destroys the fibers and forms brittle Al4C3. Join with mechanical fasteners using titanium or aluminum bushings, adhesive bonding, or low-temperature vacuum brazing and diffusion bonding, with galvanic isolation at the interfaces.

Can P100Gr/6061Al be formed, bent or molded?

Near-net shape only: aluminum foil and fiber stacks are vacuum hot pressed and diffusion bonded, or pressure-infiltration cast with tight control of temperature and hold time to suppress interface reaction. Consolidated parts cannot be cold bent or reformed.

What surface finishes work on P100Gr/6061Al?

Seal all edges and cut-outs and protect the whole part with ion vapor deposited aluminum, nickel plating, chemical conversion coating or paint. Galvanic corrosion between bare graphite and aluminum is the main failure source; space parts add low-outgassing and thermal-control coatings.

P100Gr/6061Al 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
P100 pitch-based graphite fiberwt%; 40–55 vol%; fiber modulus ~760 GPa; axial CTE ~-1.4 µm/m·K34 – 5039
Mg6061 matrix composition (matrix basis, GB/T 3190 / AA)0.8 – 1.21
Simatrix basis0.4 – 0.80.6
Cumatrix basis0.15 – 0.40.28
Crmatrix basis0.04 – 0.350.2
Feimpurity limit, matrix basis≤ 0.70.3
Mnmatrix basis≤ 0.150.05
Znmatrix basis≤ 0.250.05
Timatrix basis≤ 0.150.03
Albalance of 6061 matrix; ~60 wt% of the compositebalance—

P100Gr/6061Al UD45-F — frequently asked

What is P100Gr/6061Al UD45-F used for?

P100Gr/6061Al UD45-F is typically used for satellite optical benches, space truss structures and antenna support structures. In short: near-zero CTE composite; 320 GPa and 320 W/m·K; space-structure grade.

What is the tensile strength of P100Gr/6061Al UD45-F?

P100Gr/6061Al UD45-F has a typical tensile strength of 620 MPa (89.9 ksi) — stronger than 69% of composite grades. Strength varies by condition: see the 5 listed tempers.

Is P100Gr/6061Al UD45-F easy to machine?

Not especially — machinability is rated not recommended (12/100, worse than 89% of composite grades). Requires PCD or CVD-diamond tooling at high speed and low feed with full coolant to avoid fiber pull-out and delamination. Use water-guided laser or diamond grinding for holes and edge trimming; ordinary carbide tool life is extremely short.

Can P100Gr/6061Al UD45-F be welded?

Not fusion weldable — the weld pool destroys the fibers and forms brittle Al4C3. Join with mechanical fasteners using titanium or aluminum bushings, adhesive bonding, or low-temperature vacuum brazing and diffusion bonding, with galvanic isolation at the interfaces.

What surface finishes work on P100Gr/6061Al UD45-F?

Seal all edges and cut-outs and protect the whole part with ion vapor deposited aluminum, nickel plating, chemical conversion coating or paint. Galvanic corrosion between bare graphite and aluminum is the main failure source; space parts add low-outgassing and thermal-control coatings.

Can P100Gr/6061Al UD45-F be formed, bent or molded?

Near-net shape only: aluminum foil and fiber stacks are vacuum hot pressed and diffusion bonded, or pressure-infiltration cast with tight control of temperature and hold time to suppress interface reaction. Consolidated parts cannot be cold bent or reformed.

What is the maximum service temperature of P100Gr/6061Al UD45-F?

P100Gr/6061Al UD45-F is rated for continuous use to about 350°C (662 °F), and briefly to 450°C. Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between P100Gr/6061Al UD45-F and P100Gr/6061Al UD55-F?

UD45-F is the default condition — standard unidirectional Vf≈45% plate in as-fabricated condition: near-zero axial expansion and 320 GPa modulus suit truss struts and other one-dimensional load paths, with only 0.3 % elongation. UD55-F: pick for maximum axial stiffness (400 GPa), 380 W/m·K conduction and near-zero or negative CTE; at ~55% fibre volume the transverse and shear properties drop further.

Sources

  1. ASM Handbook Vol.21: Composites — Metal Matrix Composites — ASM International (2001)
  2. MIL-HDBK-17 / CMH-17 Vol.4: Metal Matrix Composites — US DoD / SAE (2002)
  3. Thornel P-100 Pitch-Based Carbon Fiber Data Sheet — Cytec / Solvay (formerly Amoco) (2012)
  4. Aluminum Standards and Data (6061 matrix composition) — The Aluminum Association (2015)
  5. Graphite/Aluminum composite structural test reports — NASA / AFML technical reports (1990)

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.