 |
環氧樹脂 | |
| 耐燒蝕酚醛樹脂 | ||
| 矽樹脂 | ||
| 聚醯亞胺樹脂 | ||
| . | . | |
| Resin | Features & Benefites | Applications | Minimum Cure Temp | Service Temp | Cure Methods | Notes |
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| P600 |
Low cost, General purpose grade, Low temperature cure, Non-styrenated/Low VOC, Effective replacement for wet lay-up |
Structural, Industrial parts |
180°F- 250°F |
160°F | V,A,C |
Meets |
| P601 | Flame retardant version of P600 | Geodesic radomes, Shelters, Industrial parts | ||||
| P605 | Designed for tube rolling applications, Non-styrenated/Low VOC | Poles and shafts | ||||
| P650M | Modified diallyphthallate, Excellent wet electrical properties, Non-styrenated/Low VOC | Aircraft structures, Electrical applications |
250°F- 300°F |
250°F |
Meets Mil-R-7575C- Grade A, Aerospace qualified |
|
| P650R | Designed for optical clarity, Good mechanical and electrical properties, Non-styrenated/Low VOC | Applications which require optical clarity, Aircraft lighting, etc. | ||||
| P670I | High service temperature, Flame retardant, Excellent electrical and mechanical properties, Non-styrenated/Low VOC | Aircraft structures, Radomes | to 350°F |
Meets Mil-R-7575C- Grade A & B, Aerospace qualified |
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| E717 | Self adhesive, High peel strength, Controlled flow, Flame retardant, Low tack, Good handleability for large panels | Sandwich panels or solid laminates |
250°F- 325°F |
265°F | A,C |
Meets Mil-R-9300B- Type I, Meets FAR 25.853, Aerospace qualified |
| E746 | Designed for high temperature service, Structural grade, Excellent hot/wet properties, Extensive database | Aircraft structures, Radomes |
300°F- 350°F |
to 500°F |
Meets Mil-R-9300B- Type II, Aerospace qualified |
|
| E761 | Self-adhesive, Flame retardant, Controlled flow, Good electrical properties, Extensive database, Versatile processing, Long out-time | Solid laminates or sandwich panels, Radomes |
180°F- 275°F |
to 200°F | V,A,C |
Meets Mil-R-9300B- Type I, Meets FAR 25.853, Aerospace qualified |
| E763 | Good clarity, Versatile processing, Long out-time | Aircraft structures, Industrial & Recreation parts where clarity is desired |
180°F- 300°F |
to 200°F |
Meets Mil-R-9300B- Type I, Aerospace qualified |
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| E765 | Tough, 250°F cure system designed to replace many first generation 350°F systems, Extensive FAA Approved Databases, Versatile processing, Long out-time | Aircraft primary and secondary structures |
250°F- 300°F |
to 275°F | FAA approved databases, Aerospace qualified | |
| E766 | Self-adhesive, High peel strength, Flame retardant, Controlled flow, Good electrical properties, Extensive database, Versatile processing, Long out-time | Solid laminates or sandwich panels, Radomes |
250°F- 300°F |
to 200°F |
Meets Mil-R-9300B- Type I, Meets FAR 25.853, Aerospace qualified |
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E769 Surface Film |
Supported film used to minimize laminate surface porosity, Good tack and drape, Reduces finish labor | Any epoxy laminate where surface finish is critical |
250°F- 350°F |
to 275°F | Co-cures with most resin system, Aerospace qualified | |
| E774 | Designed for tube rolling applications, Post formable | Poles and shafts |
250°F- 300°F |
to 200°F |
Meets Mil-R-9300B- Type I |
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| E798 | High temperature structural grade, Flame retardant | Aircraft ducts | 350°F | to 375°F |
Meets Mil-R-9300B- Type II, Aerospace qualified |
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| F502 | Structural grade system, Good tack and drape, Excellent high temperature properties, Also has good ablative characteristics | Aircraft structures, Ducts, High temperature furnace chambers, Rocket nozzles |
325°F- 375°F |
500°F | A,C |
Meets Mil-R-9299C- Grade A & B |
|
F502 High Silica |
Works well in oxidative environments, Low pressure autoclave cure, Coated onto leached glass fabric style C100-48 | Liquid rocket nozzles, Combustion chambers, Blast tubes, Exit cones, Insulators |
325°F- 350°F |
N/A | ||
|
F554 High Silica |
Works well in oxidative environments, Coated onto leached glass fabric style C100-48 | Liquid rocket nozzles, Combustion chambers, Blast tubes, Exit cones, Insulators |
350°F- 400°F |
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| F555 Carbonized Rayon | Carbon loaded, Coated on continuous filiment 8HS carbonized rayon fabric, High strength | Nozzles, Exit cones | Used for large nozzles and exit cones on launch vehicles | |||
| F589 PAN | Carbon loaded, Coated on continuous filiment 6K 5HS Part Fabric, High Strenght | Aft exit cones | Substitute for rayon where higher CTE and higher thermal expansion can be tolerated | |||
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*Ablative materials are available in broadgood, bias tape and chopped forms
Silicones |
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| S-860 | Excellent high temperatures properties | Aircraft structures | 350°F | 500°F | A,C |
Meets Mil-P-25518 Aerospace qualified |
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| V376 Cyanate Ester | Cost effective cyanate ester, Easy to process, Excellent electrical and hot/wet mechanical properties | High performance radomes, Low observables |
300°F- 350°F |
to 400°F | A,C | D/C 3.2, Loss 0.004 (Quartz) |
| V341 Polybutidiene | Excellent electrical properties, Good mechanical properties | 350°F | to 200°F | D/C 3.1, Loss 0.001 (Quartz) | ||
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| Peel Cote™ | Prepregged nylon peel-ply, Excellent mold-side peel-ply to improve laminate surface quality and as a preparation for bonding and painting operations, Reduce finish labor | Most prepreg applications |
250°F
or 350°F |
N/A | V,A,C | Several 250°F and 350°F epoxy systems available |
| Corefix™ | Disposable prepreg used to stabilize honeycomb materials during handling and machining, Several advantages over traditional prepregs and double-backed tapes | Honeycomb machining aid | N/A | N/A | V,C | Can be stored at room temp. |
| E769 Surface Film | Supported film used to minimize laminate surface porosity, Good tack and drape, Reduces finish labor | Any epoxy laminate where surface finish is critical |
250°F- 350°F |
to 275°F | V,A,C | Co-cures with most resin systems, Aerospace qualified |
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