Solvay Cycom 977-2 Toughened Aerospace Carbon Epoxy Prepreg vs. Toray Torayca T700S 12K Unidirectional Carbon Fabric
Solvay Cycom 977-2 Toughened Aerospace Carbon Epoxy Prepreg (Syensqo / Solvay Composite Materials) and Toray Torayca T700S 12K Unidirectional Carbon Fabric (Toray Composite Materials America) achieve a 83.8% ASTM engineering compatibility score in Carbon Fiber Fabrics (3K / 6K / 12K), Spread-Tow & Prepregs. Tensile strength delta is -2210 MPa (-45.1%) and thermal HDT delta is matched, making them interchangeable with post-cure temperature and viscosity flow adjustments.
Side-by-Side ASTM Mechanical, Thermal, Rheological & Pricing Delta
| ASTM Parameter | A: Solvay Cycom 977-2 Toughened Aerospace Carbon Epoxy Prepreg (Syensqo / Solvay Composite Materials) | B: Toray Torayca T700S 12K Unidirectional Carbon Fabric (Toray Composite Materials America) | Engineering Delta (A vs. B) |
|---|---|---|---|
| OEM Manufacturer & SKU | Syensqo / Solvay Composite Materials • SLV-CYC977-2 | Toray Composite Materials America • TOR-T700S-300GSM | Cross-Brand OEM Equivalent |
| ASTM D638 Tensile Strength (MPa / PSI) | 2690 MPa (390,152 psi) | 4900 MPa (710,686 psi) | -2210 MPa (-45.1 %) |
| ASTM D648 Heat Deflection Temp (HDT °C / °F) | N/A | N/A | Ambient / N/A |
| ASTM D790 Flexural Strength (MPa) | 1760 MPa | N/A | N/A |
| ASTM D2583 Barcol Hardness | N/A | N/A | N/A |
| ASTM D2196 Brookfield Viscosity @ 25°C | Solid Reinforcement / Core | Solid Reinforcement / Core | Solid State |
| Gel Time @ 25°C (Minutes) | N/A | N/A | N/A |
| ASTM D792 Specific Density (kg/m³) | 1790 kg/m³ | 1800 kg/m³ | -10 kg/m³ |
| US DOT 49 CFR & TDG Hazmat Class | Non-Regulated Industrial Fiber (N/A) | Non-Regulated (N/A) | Identical (N/A) |
| Unit Price ($/kg USD) & Pack Price | $136/kg • $6,120 (100 yd Roll (45 kg)) | $39.5/kg • $2,680 (100 yd Roll (50" Wide, 300 gsm)) | +96.5 $/kg (+244.3 %) |
| US Stocking Warehouses | Tacoma, WA • Stamford, CT • Anderson, SC | Tacoma, WA • Santa Fe Springs, CA • Decatur, AL | 1–3 Days LTL Dispatch |
Companion process stack: Low-Viscosity Infusion Epoxy (Gurit Prime 37 / Hexion RIMR 135 / Araldite LY 1564) + Stoichiometric Amine Hardener. Follow SIZE COMPATIBILITY: Use Epoxy-compatible silane sizing with Structural Epoxy Resins (approx. 55:45 fiber-to-resin weight ratio in vacuum infusion). ITAR/EAR export screening applies.
Direct Drop-In Qualified: Thermal deflection (ASTM D648 HDT) differs by only 0 °C (N/A °C vs. N/A °C). Existing mold cure and demold cycles can be maintained without thermal schedule modification.
Identical Hazmat Logistics Profile: Both SKUs ship under US DOT 49 CFR & Transport Canada TDG as Non-Regulated Industrial Fiber (UN Number: N/A). Note 49 CFR § 177.848 segregation if ordering with Class 5.2 Organic Peroxides (UN3105).
Engineering FAQ: Solvay Cycom 977-2 Toughened Aerospace Carbon Epoxy Prepreg vs. Toray Torayca T700S 12K Unidirectional Carbon Fabric
1. Is Solvay Cycom 977-2 Toughened Aerospace Carbon Epoxy Prepreg a direct drop-in equivalent for Toray Torayca T700S 12K Unidirectional Carbon Fabric?▼
Solvay Cycom 977-2 Toughened Aerospace Carbon Epoxy Prepreg (Syensqo / Solvay Composite Materials) and Toray Torayca T700S 12K Unidirectional Carbon Fabric (Toray Composite Materials America) achieve a 83.8% ASTM engineering compatibility score in Carbon Fiber Fabrics (3K / 6K / 12K), Spread-Tow & Prepregs. Tensile strength delta is -2210 MPa (-45.1%) and thermal HDT delta is matched, making them interchangeable with post-cure temperature and viscosity flow adjustments.
2. What is the ASTM D638 Tensile Strength and ASTM D648 HDT difference between Solvay Cycom 977-2 Toughened Aerospace Carbon Epoxy Prepreg and Toray Torayca T700S 12K Unidirectional Carbon Fabric?▼
Solvay Cycom 977-2 Toughened Aerospace Carbon Epoxy Prepreg (Syensqo / Solvay Composite Materials) delivers ASTM D638 Tensile Strength of 2690 MPa (390,152 psi) and ASTM D648 HDT of N/A °C, whereas Toray Torayca T700S 12K Unidirectional Carbon Fabric (Toray Composite Materials America) delivers 4900 MPa (710,686 psi) and HDT of N/A °C. The net delta is -2210 MPa (-45.1 %) tensile and N/A HDT.
3. Do Solvay Cycom 977-2 Toughened Aerospace Carbon Epoxy Prepreg and Toray Torayca T700S 12K Unidirectional Carbon Fabric use the same catalyst or hardener cure system?▼
Companion process stack: Low-Viscosity Infusion Epoxy (Gurit Prime 37 / Hexion RIMR 135 / Araldite LY 1564) + Stoichiometric Amine Hardener. Follow SIZE COMPATIBILITY: Use Epoxy-compatible silane sizing with Structural Epoxy Resins (approx. 55:45 fiber-to-resin weight ratio in vacuum infusion). ITAR/EAR export screening applies. Direct Drop-In Qualified: Thermal deflection (ASTM D648 HDT) differs by only 0 °C (N/A °C vs. N/A °C). Existing mold cure and demold cycles can be maintained without thermal schedule modification.
4. How do US DOT 49 CFR Hazmat shipping rules and B2B drum/pack prices compare between Solvay Cycom 977-2 Toughened Aerospace Carbon Epoxy Prepreg and Toray Torayca T700S 12K Unidirectional Carbon Fabric?▼
Identical Hazmat Logistics Profile: Both SKUs ship under US DOT 49 CFR & Transport Canada TDG as Non-Regulated Industrial Fiber (UN Number: N/A). Note 49 CFR § 177.848 segregation if ordering with Class 5.2 Organic Peroxides (UN3105). In US B2B distribution, Solvay Cycom 977-2 Toughened Aerospace Carbon Epoxy Prepreg is priced at $6,120 per 100 yd Roll (45 kg) ($136/kg) vs. $2,680 per 100 yd Roll (50" Wide, 300 gsm) ($39.5/kg) for Toray Torayca T700S 12K Unidirectional Carbon Fabric (delta: +96.5 USD/kg).
Related Drop-In Comparisons in Carbon Fiber Fabrics (3K / 6K / 12K), Spread-Tow & Prepregs
Solvay Cycom 977-2 Toughened Aerospace Carbon Epoxy Prepreg (Syensqo / Solvay Composite Materials) and Toray Torayca T700S 12K Unidirectional Carbon Fabric (Toray Composite Materials America) are trademarks of their respective owners. CompositeMatrix Technologies Inc. is an independent North American B2B composite material intelligence registry; comparative ASTM D638, D648, D790, D2583, and D2196 figures are presented under the US legal doctrine of Nominative Fair Use (Lanham Act, 15 U.S.C. § 1125) and Feist Publications, Inc. v. Rural Telephone Service Co. (499 U.S. 340) for scientific and industrial cross-reference. Cure schedules, exotherm behavior, and laminate qualification must be verified by a licensed Naval Architect or Professional Engineer (PE) against current manufacturer batch Technical Data Sheets (TDS) and Safety Data Sheets (SDS).