E-752-LT Epoxy Prepreg Product Overview Park s E 752 LT is a toughened; 350 F (177 C) cure epoxy resin system with 315 F (157 C) wet Tg for primary and secondary structural applications. E 752 LT is formulated for efficient processing in high volume Automated Fiber Placement (AFP) applications manufacturing. The resin system offers a combination of toughness, low moisture uptake and good mechanical properties. E 752 LT is formulated to laminate In Autoclave (AC), Out of Autoclave (OOA) and Press cure conditions. Key Features & Benefits Toughened epoxy for primary and secondary aerospace structures Specifically designed for efficient AFP processing Controlled flow rheology specifically designed to facilitate a wide range of processing for AC, OOA and Press cures Processes in OOA without the need for extensive bagging and pre vacuum procedures Wet DMA Tg of 315 F (157 C) Dry DMA Tg of 428 F (220 C) Capable of low laminate void content < 1% Product Forms Applications / Qualifications Primary and Secondary Aerospace Structures fabricated with AFP processes Wings / Control Surfaces / Airframes Turbofan Engine Components Nacelles/ Fan Reversers Air Ducting Fairings Global Availability For information about Park s materials: Americas +1 316 283 6500 Asia Pacific +65 6861 7117 Europe +33 5 62 98 52 90 Web Email www.parkelectro.com info@parkelectro.com Available AFP product forms o 0.125 +/ 0.005 (3.18 mm +/ 0.13 mm) o 0.250 +/ 0.005 (6.35 mm +/ 0.13 mm) Unidirectional (UD) Tape up to 48 (1.2 m) width Woven fabric prepreg up to 60 (1.5 m) width Page 1 of 6 Rev. 02 13 15
E-752-LT Epoxy Prepreg Reinforcement HTS45 AS4 GP IMS65 HTS40 HTS40 12K 12K 24K 3K8HS 3KPW UD Tape UD Tape UD Tape Fabric Fabric Fabric Area Weight (gsm) 145±5 145±5 145 ±5 370±5 193±8 Prepreg Resin Content (%) 35±2 35±2 33±2 37±2 38±3 Resin Flow (350 F/177 C, 50psi) (%) 8 20 8 20 8 20 8 20 8 20 Note: Flow values are for general guidance and may change per customer specifications Other fiber types and product forms are available upon request Test data represents typical values and is not intended to be used for customer specifications AFP Laid up Panels, Autoclave HTS45E23/E 752 LT @ 35% RC, 145 gsm FAW 0 Tensile Strength [0 ] 8 RTA ASTM D3039 ksi Mpa 325 2243 0 Tensile Modulus [0 ] 8 RTA ASTM D3039 msi GPa 19.8 136.6 0 Compressive Strength [0 ] 8 RTA SRM 1R 94 ksi MPa 242 1668 0 Compressive Modulus [0 ] 8 RTA SRM 1R 94 msi GPa 17.1 117.9 90 Compressive Strength [0 ] 16 RTA SRM 1R 94 ksi MPa 49.5 341 90 Compressive Modulus [0 ] 16 RTA SRM 1R 94 msi GPa 1.4 10.0 ±45 Inplane Shear Strength* [±45 ] 2s RTA ASTM D3518 ksi Mpa 12.6 87 ±45 Inplane Shear Modulus [±45 ] 2s RTA ASTM D3518 msi GPa 0.6 4.3 Open Hole Tensile Strength ([0 /45/90/ 45] s ) 2 RTA ASTM D5766 ksi Mpa 53.5 369 Open Hole Tensile Modulus ([0 /45/90/ 45] s ) 2 RTA ASTM D5766 msi GPa 7.5 51.9 Autoclave Cure Cycle: 3 F/min to 350 F, 2 hrs at 350 F at 45psi and full vacuum Normalized to 5.6 mil CPT except for IPS *IPS value reported at 5% strain Compressive, Tensile and OHT are reported average of 3 lots Page 2 of 6 Rev. 02 13 15
E 752 LT @ 35% RC, 130 gsm FAW, Autoclave HTS40E13 AS4 GP RTD 312 2151 299 2061 0 Tensile Strength [0 ] 8 75 F CTD 300 2068 306 2110 250 F RTD 338 2330 298 2054 250 F ETW ASTM D3039 ksi MPa 284 1958 281 1937 RTD 10.6 73 11.6 80 90 Tensile Strength [0 ] 16 75 F CTD 11.0 76 12.3 85 250 F ETW 5.7 40 6.0 41 RTD 18.6 128.6 18.1 125.2 0 Tensile Modulus [0 ] 8 75 F CTD 17.2 118.9 18.2 125.9 250 F Dry 20.2 139.7 17.9 123.8 250 F ETW ASTM D3039 msi GPa 17.8 123.1 18.6 128.6 RTD 1.2 8.6 1.3 8.6 90 Tensile Modulus [0 ] 16 75 F CTD 1.4 9.5 1.4 9.5 250 F ETW 0.8 5.2 0.8 5.5 RTD 219 1510 188 1296 75 F CTD 234 1613 254 1751 0 Compressive Strength [0 ] 8 250 F RTD 179 1234 208 1434 250 F Humid SRM 1R 94 ksi MPa 170 1172 160 1103 RTD MEK 227 1565 231 1593 90 Compressive Strength [0 ] 8 RTD 42 290 42 290 250 F ETW 22 152 23.6 163 RTD 18.7 129.3 16.1 111.3 75 F CTD 18.8 130.0 18.0 124.5 0 Compression Modulus [0 ] 10 250 F RTD 16.8 116.2 18.8 130.0 250 F ETW SRM 1R 94 msi GPa 14.4 99.6 16.2 112.0 RTD MEK 16.0 110.6 17.3 119.6 90 Compression Modulus [0 ] 10 RTD 1.6 10.7 1.5 10.6 250 F ETW 0.9 6.3 0.9 6.4 RTD 12.3 *1 84.8 12.94 *1 89.2 ±45 Inplane Shear Strength [+45 / 45 ] 75 F CTD 18.0 *2 124.1 17.8 *2 4s ASTM D3518 ksi MPa 122.7 250 F ETW 13.6 *2 93.8 14.0 *2 96.5 RTD 0.7 4.6 0.7 5.0 ±45 Inplane Shear Moduls [+45 / 45 ] 4s 75 F CTD ASTM D3518 msi GPa 0.8 5.6 0.9 5.9 250 F ETW 0.4 2.6 0.4 2.7 Interlaminar Shear Strength G 1c [0 ] 50 RTD ASTM D2344 ksi MPa 14.6 *3 101 13.0 *3 89.6 [0 ] 36 RTD ASTM D5528 in psi kj/m 2 0.8 0.14 1.2 0.21 Open Hole Tensile Strength Open Hole Tensile Modulus Open Hole Compressive Strength Open Hole Compressive Modulus [+45 /0 / 45 /90 ] 3S [+45 /0 / 45 /90 ] 3S [+45 /0 / 45 /90 ] 4S [+45 /0 / 45 /90 ] 4S RTD 54.1 373 52.4 361 ASTM D5766 ksi MPa 75 F CTD 56.9 392 51.3 354 RTD 7.0 48.4 7.4 51.2 ASTM D5766 msi GPa 75 F CTD 7.7 53.2 7.9 54.6 RTD 48.0 331 51.7 356 ASTM D6484 ksi MPa 250 F ETW 40.4 279 39.2 270 RTD 6.7 46.3 6.8 47.0 ASTM D6484 msi GPa 250 F ETW 6.9 47.7 6.8 47.0 Compression After Impact [+45 /0 / 45 /90 ] 4S RTD SRM 2R094 ksi MPa 24.4 168 23.4 161 Autoclave Cure Cycle: 3 F/min to 350 F, 2 hrs at 350 F at 45psi and full vacuum Normalized to 57.9% V f except for 90 lamina properties, IPS, ILSS, G 1c and CAI *1 IPS value reported at 5% strain *2 IPS value reported at failure strength *3 At 6:1 span: mixed failure modes ETW: Saturated at 160 F/85%RH to equlibrium and then tested at 250 F 5 10 minutes after reaching equlibrium Page 3 of 6 Rev. 02 13 15
IMS65E23/E 752 LT @ 33% RC, 145 gsm FAW, OOA 0 Tensile Strength [0 ] 8 RTA ASTM D3039 ksi MPa 422 2909 0 Tensile Modulus [0 ] 8 RTA ASTM D3039 msi GPa 23.4 161.7 0 Compressive Strength [0 ] 8 RTA SRM 1R 94 ksi MPa 235 1619 0 Compressive Modulus [0 ] 8 RTA SRM 1R 94 msi GPa 21.2 146.5 90 Compressive Strength [0 ] 16 RTA SRM 1R 94 ksi MPa 44.6 307 90 Compressive Modulus [0 ] 16 RTA SRM 1R 94 msi GPa 1.5 10.2 0 /90 Compressive Strength [0 /90 ] 2s RTA SRM 1R 94 ksi MPa 147 1016 0 /90 Compressive Modulus [0 /90 ] 2s RTA SRM 1R 94 msi GPa 11.8 81.3 0 Intelaminar Strength [0 ] 16 RTA ASTM D2344 ksi MPa 17.9 123 ±45 Inplane Shear Strength* [±45 ] 2s RTA ASTM D3518 ksi MPa 12.7 88 ±45 Inplane Shear Modulus [±45 ] 2s RTA ASTM D3518 msi GPa 0.7 4.8 Open Hole Tensile Strength [0 /45 /90 / 45 ] 3s RTA ASTM D5766 ksi MPa 88 606 Open Hole Tensile Modulus [0 /45 /90 / 45 ] 3s RTA ASTM D5766 msi GPa 9.37 64.8 Oven Cure Cycle: 4 F/min to 265 F, 4 hrs at 265 F, 1.5 F/min to 350 F and 2 hrs at 350 F at 27ʺ Hg Normalized to 5.4 mil CPT except for SBS and IPS *IPS value reported at 5% strain HTS40E13 3K8HS /E 752 LT @ 37% RC, 370 gsm FAW, OOA 0 Tensile Strength [0 ] 8 RTA ASTM D3039 ksi MPa 152 1045 0 Tensile Modulus [0 ] 8 RTA ASTM D3039 msi GPa 9.9 88.3 90 Tensile Strength [0 ] 8 RTA ASTM D3039 ksi MPa 139 956 90 Tensile Modulus [0 ] 8 RTA ASTM D3039 msi GPa 9.5 84.7 0 Compressive Strength [0 ] 16 RTA ASTM D6641 ksi MPa 116 802 0 Compressive Modulus [0 ] 16 RTA ASTM D6641 msi GPa 9.1 81.1 0 Compressive Strength [0 /90 ] 2s RTA ASTM D6641 ksi MPa 116 801 0 Compressive Modulus [0 /90 ] 2s RTA ASTM D6641 msi GPa 9.3 82.9 0 Intelaminar Strength [0 ] 16 RTA ASTM D2344 ksi MPa 10.7 74 ±45 Inplane Shear Strength* [±45 ] 2s RTA ASTM D3518 ksi MPa 13.3 92 ±45 Inplane Shear Modulus [±45 ] 2s RTA ASTM D3518 msi GPa 0.7 6.2 Open Hole Tensile Strength [0 /45 /90 / 45 ] s RTA ASTM D5766 ksi MPa 61 419 Open Hole Tensile Modulus [0 /45 /90 / 45 ] s RTA ASTM D5766 msi GPa 7.1 63.5 Oven Cure Cycle: 4 F/min to 265 F, 4 hrs at 265 F, 1.5 F/min to 350 F and 2 hrs at 350 F at 27ʺ Hg Normalized to 5.4 mil CPT except for SBS and IPS *IPS value reported at 5% strain Page 4 of 6 Rev. 02 13 15
HTS40E13 3KPW /E 752 LT @ 38% RC, 193 gsm FAW, Autoclave 0 Tensile Strength [0 ] 14 0 Tensile Strength [0 ] 14 0 Tensile Modulus [0 ] 14 90 Tensile Modulus [0 ] 14 RTD 148 1020 75 F CTD 150 1034 250 F RTD 153 1055 250 F ETW ASTM D3039 ksi MPa 130 896 RTD 137 944 75 F CTD 132 910 250 F ETW 116 800 RTD 9.3 64 75 F CTD 9.5 66 250 Dry 9.2 64 250 F ETW ASTM D3039 msi GPa 8.8 61 RTD 9.1 63 75 F CTD 9.2 64 250 F ETW 9.1 63 RTD 140 962 250 F RTD 114 786 0 Compressive Strength [0 ] 16 250 Humid ASTM D3039 ksi MPa 75 517 RTD MEK 107 738 90 Compressive Strength [0 ] 16 RTD 111 765 RTD 8.7 60 75 F CTD 8.4 58 0 Compression Modulus [0 ] 16 250 F RTD 8.8 61 250 F ETW ASTM D3039 msi GPa 8.6 59 90 Compression Modulus [0 ] 16 RTD MEK 8.4 58 RTD 8.7 60 250 F ETW 8.8 61 RTD 18.2 *1 125 ±45 Inplane Shear Strength [+45 / 45 ] 75 F CTD 17.9 *2 2s ASTM D3518 ksi MPa 123 250 F ETW 10.9 *2 75 RTD 0.7 5 ±45 Inplane Shear Moduls [+45 / 45 ] 2s 75 F CTD ASTM D3518 msi MPa 1.0 7 Interlaminar Shear Strength G 1c 250 F ETW 0.4 3 [0 ] 24 RTD ASTM D2344 ksi GPa 13.2 *3 91 [0 ] 22 RTD ASTM D5528 in psi kj/m 2 2.7 0.47 RTD 53.1 366 Open Hole Tensile Strength [+45 /0 / 45 /90 ] 2S ASTM D5766 ksi MPa 75 F CTD 53.6 370 RTD 6.9 48 Open Hole Tensile Modulus [+45 /0 / 45 /90 ] 2S ASTM D5766 msi GPa 75 F CTD 7.4 51 RTD 45.8 316 Open Hole Compressive Strength [+45 /0 / 45 /90 ] 2S ASTM D6484 ksi MPa 250 F ETW 33.9 234 RTD 6.7 46 Open Hole Compressive Modulus [+45 /0 / 45 /90 ] 2S ASTM D6484 msi GPa 250 F ETW 6.0 41 Compression After Impact Autoclave Cure Cycle: 3 F/min to 350 F, 2 hrs at 350 F at 45psi and full vacuum [+45 /0 / 45 /90 ] 2S RTD SRM 2R094 ksi MPa 34 234 Normalized to 54.42% V f except for 90 lamina properties, IPS, ILSS, G 1c and CAI *1 IPS value reported at 5% strain *2 IPS value reported at failure strength *3 At 6:1 span: mixed failure modes ETW: Saturated at 160 F/85%RH to equlibriumand then tested at 250 F 5 10 minutes after reaching equlibrium Page 5 of 6 Rev. 02 13 15
Processing Guideline Prepreg Storage Life Tack Life: Contact Park Engineering Out Life: Contact Park Engineering Shelf Life: 12 months @ 0 F ( 18 C) Note: The following guidelines are provided to assist the users of Park materials with general recommendations for successful processing. The recommendations are for general review purposes only and process adjustments may be required to achieve optimum results in your specific manufacturing environment. Consult Park s Technical Engineering for recommendations. E 752 LT Cure Scan Rheology 0.05% Strain, 1Hz 5 C/min Wide Process Controlled Flow Window Autoclave Cure Apply full vacuum (27in / 686mm Hg typical) and pressure of 30±5 psig (2.0 bar). Ramp Temperature at 1 4 F (0.6 2.2 C)/min to 350 F ± 5 F (177 C ± 2.8 C). When leading thermocouple reaches 225 F (107 C), vent vacuum to atmosphere and increase pressure to 45±5 psig (6.2±.35 bar). Dwell at 350 F (177 C) for 120±10 minutes (dwell time begins when lagging thermocouple reaches 340 F / 171 C). Out of Autoclave Cure Apply full vacuum (27in / 686mm Hg typical) for 5 minutes minimum prior to heat up. Ramp Temperature at 1 4 F (0.6 2.2 C)/min to 265 F ± 5ºF (129 C ± 2.8 C). Dwell at 265 ±5 F (129 C ± 2.8 C) for 260±10 minutes (dwell time begins when lagging thermocouple reaches 260 F / 127 C). Ramp down at <8ºF (4.4 ºC)/minute. Remove panels after temperature is below 120 F (49 C). Ramp down at 4 F (2.2 C) / minute. Release pressure after temperature is below 150 F (66 C). Remove panels after temperature is below 120 F (49 C). Out of Autoclave Cure Post Cure Oven Ramp Temperature at 1 4 F (0.6 2.2 C)/min to 265 F ± 5 F (129 C ± 2.8 C). Ramp Temperature at 1 2 F (0.6 1.1 C)/min to 350 F ± 5 F (177± 2.8 C). Dwell at 350ºF (177 C) for 120±10 minutes (dwell time begins when lagging thermocouple reaches 345 F / 174 C). Ramp down at <8 F (4.4 C)/minute. Remove panels after temperature is below 120 F (49 C). Page 6 of 6 Rev. 02 13 15