Composite Panel Data for FEA Modeling

COMPOSITE PANEL DATA SHEETUNI INNEGRA™ S / UNI CARBON FIBER PREPREG PANELPANEL CONSTRUCTION MATERIALS [IUD] Innegra Unitape Prepreg - Axiom Ax-6200-I-150: 4.4 oz/yd2 (150 gsm) [CUD] Carbon T-700 Unitape Prepreg - Axiom AX-6200-T700: 4.4 oz/yd2 (150 gsm) LAYUP • Ply Schedule: [C] 2 PLY / [I] 1 PLY/ [C] 2 PLY / [I] 1 PLY / [C] 2 PLY • Cure Cycle: Apply 10-50 psi (0.69-3.45 bar), Ramp RT to 250°F (121°C) at 2-4°F/ minute (1-2°C/minute). Hold 60 minutes at 250°F (121°C). Cool to 180°F (82°C) or below and remove pressure. • Resin content: 38% ±3 by volume All testing performed by a NADCAP accredited...

COMPOSITE PANEL DATA SHEETINNEGRA™ S / 282 CARBON FIBER PREPREG PANELPANEL CONSTRUCTION MATERIALS [I] Innegra™ S fabric - 940 Denier 3.6 oz/yd2 (122gsm) plain weave / Axiom Ax-3201M Prepreg [C] Carbon Fiber fabric - Style 282 3K (5.8 oz/yd2 (196 gsm) plain weave / Axiom Ax-5201M Prepreg LAYUP • Ply Schedule: [C] 2 ply / [I] 6 ply / [C] 2 ply • Cure Cycle: Apply 10-50 psi (0.69-3.45 bar), Ramp RT to 250°F (121°C) at 2-4°F/ minute (1-2°C/minute). Hold 60 minutes at 250°F (121°C). Cool to 180°F (82°C) or below and remove pressure. • Resin content: 38% ±3 by volume All testing performed by a NADCAP...

COMPOSITE PANEL DATA SHEET282 CARBON FIBER PREPREG FOAM CORE PANELPANEL CONSTRUCTION MATERIALS [C] Carbon Fiber fabric - Style 282 3K (5.8 oz/yd2 (196 gsm) plain weave / Axiom Ax-5201M Prepreg [D] Divinycell HP 60 foam LAYUP • Ply Schedule: [C] 3 ply / [D] foam / [C] 3 ply • Cure Cycle: Apply 10-50 psi (0.69-3.45 bar), Ramp RT to 250°F (121°C) at 2-4°F/ minute (1-2°C/minute). Hold 60 minutes at 250°F (121°C). Cool to 180°F (82°C) or below and remove pressure. • Resin content: 38% ±3 by volume All testing performed by a NADCAP accredited laboratory. INNEGRA TECHNOLOGIES, LLC 270 Feaster Road Greenville,...

COMPOSITE PANEL DATA SHEETINNEGRA™ S / 282 CARBON FIBER PREPREG PANELPANEL CONSTRUCTION MATERIALS [I] Innegra™ S fabric - 940 Denier 3.6 oz/yd2 (122gsm) plain weave / Axiom Ax-3201M Prepreg [C] Carbon Fiber fabric - Style 282 3K (5.8 oz/yd2 (196 gsm) plain weave / Axiom Ax-5201M Prepreg LAYUP • Ply Schedule: [C] 4 ply / [I] 1 ply • Cure Cycle: Apply 10-50 psi (0.69-3.45 bar), Ramp RT to 250°F (121°C) at 2-4°F/ minute (1-2°C/minute). Hold 60 minutes at 250°F (121°C). Cool to 180°F (82°C) or below and remove pressure. • Resin content: 38% ±3 by volume All testing performed by a NADCAP accredited...

COMPOSITE PANEL DATA SHEETINNEGRA™ S / 282 CARBON FIBER PREPREG PANELPANEL CONSTRUCTION MATERIALS [I] Innegra™ S fabric - 940 Denier 3.6 oz/yd2 (122gsm) plain weave / Axiom Ax-3201M Prepreg [C] Carbon Fiber fabric - Style 282 3K (5.8 oz/yd2 (196 gsm) plain weave / Axiom Ax-5201M Prepreg LAYUP • Ply Schedule: [C] 4 ply / [I] 2 ply / [C] 4 ply • Cure Cycle: Apply 10-50 psi (0.69-3.45 bar), Ramp RT to 250°F (121°C) at 2-4°F/ minute (1-2°C/minute). Hold 60 minutes at 250°F (121°C). Cool to 180°F (82°C) or below and remove pressure. • Resin content: 38% ±3 by volume All testing performed by a NADCAP...

COMPOSITE PANEL DATA SHEETUNI CARBON FIBER PREPREG PANELPANEL CONSTRUCTION MATERIALS [CUD] Carbon T-700 Unitape Prepreg - Axiom AX-6200-T700: 4.4 oz/yd2 (150 gsm) LAYUP • Ply Schedule: [C] 8 ply • Cure Cycle: Apply 10-50 psi (0.69-3.45 bar), Ramp RT to 250°F (121°C) at 2-4°F/ minute (1-2°C/minute). Hold 60 minutes at 250°F (121°C). Cool to 180°F (82°C) or below and remove pressure. • Resin content: 38% ±3 by volume All testing performed by a NADCAP accredited laboratory. INNEGRA TECHNOLOGIES, LLC 270 Feaster Road Greenville, SC 29615 • +1 864-631-2800 office • +1 864-631-2802 fax • [email protected]...

COMPOSITE PANEL DATA SHEET282 CARBON FIBER PREPREG PANELPANEL CONSTRUCTION MATERIALS [C] Carbon Fiber fabric - Style 282 3K (5.8 oz/yd2 (196 gsm) plain weave / Axiom Ax-5201M Prepreg LAYUP • Ply Schedule: [C] 10 ply • Cure Cycle: Apply 10-50 psi (0.69-3.45 bar), Ramp RT to 250°F (121°C) at 2-4°F/ minute (1-2°C/minute). Hold 60 minutes at 250°F (121°C). Cool to 180°F (82°C) or below and remove pressure. • Resin content: 38% ±3 by volume All testing performed by a NADCAP accredited laboratory. INNEGRA TECHNOLOGIES, LLC 270 Feaster Road Greenville, SC 29615 • +1 864-631-2800 office • +1 864-631-2802...

COMPOSITE PANEL DATA SHEETINNEGRA™ S / 7781 FIBERGLASS PREPREG PANELPANEL CONSTRUCTION MATERIALS [C] Carbon Fiber fabric - Style 282 3K (5.8 oz/yd2 (196 gsm) plain weave / Axiom Ax-5201M Prepreg [D] Divinycell HP 60 foam LAYUP • Ply Schedule: [C ]1 ply - [D] foam - [C] 1 ply • Cure Cycle: Apply 10-50 psi (0.69-3.45 bar), Ramp RT to 250°F (121°C) at 2-4°F/ minute (1-2°C/minute). Hold 60 minutes at 250°F (121°C). Cool to 180°F (82°C) or below and remove pressure. • Resin content: 38% ±3 by volume All testing performed by a NADCAP accredited laboratory. INNEGRA TECHNOLOGIES, LLC 270 Feaster Road...

COMPOSITE PANEL DATA SHEETINNEGRA™ S / 282 CARBON FIBER PREPREG PANELPANEL CONSTRUCTION MATERIALS [I] Innegra™ S fabric - 940 Denier 3.6 oz/yd2 (122gsm) plain weave / Axiom Ax-3201M Prepreg [C] Carbon Fiber fabric - Style 282 3K (5.8 oz/yd2 (196 gsm) plain weave / Axiom Ax-5201M Prepreg LAYUP • Ply Schedule: [C] 1 ply / [I] 2 ply / [C] 1 ply • Cure Cycle: Apply 10-50 psi (0.69-3.45 bar), Ramp RT to 250°F (121°C) at 2-4°F/ minute (1-2°C/minute). Hold 60 minutes at 250°F (121°C). Cool to 180°F (82°C) or below and remove pressure. • Resin content: 38% ±3 by volume All testing performed by a NADCAP...