Toray TC350-1

Other characteristics

Functions

Prepreg

Polymer Name

Epoxy Resins & Compounds

Processing Methods

Compression Molding, Out of Autoclave Prepreg, Vacuum Bagging

Markets

Automotive & Transportation

Shelf LIfe

Out Life

45 days at ambient

Frozen Storage Life

12 months at -18°C (< 0°F)

Out life is the maximum time allowed at ambient temperature before cure. * Ambient is 18–22°C (65–72°F).

Technology

Composite Materials

Product Handling

The following guidelines are provided to our customers to assure that best practices are used to attain the best results from Toray Advanced Composites epoxy products. Keep in mind that these procedures represent best practices for all composite prepreg and adhesive materials.; FREEZER STORAGE: Epoxy resin materials have good shelf life at room temperature; however, the life and performance of the material is best preserved with the following basic guidelines. Refer to the shelf life included in the product certifications. The epoxy material should be sealed in an airtight bag and kept frozen below -18°C (0°F) when not being used for longest life and most consistent performance. A good safety measure is to have a bag of desiccant (silica moisture absorber) in the core of the prepreg roll to assure the best protection from moisture ingression.; MOISTURE ABSORPTION AND SENSITIVITY: While very resistant to moisture absorption after cure, epoxies can be adversely affected by moisture uptake prior to cure. For this reason, all materials must be completely thawed to room temperature prior to opening the sealed bag to avoid condensation on the material. Also, it is good practice to keep prepreg and in-process hardware in a sealed bag or vacuum bag if it will be exposed to the atmosphere for long periods of time.; HANDLING OF MATERIALS: When handling any prepreg materials, one should always wear clean, powder-free latex gloves. This will assure that no hand oils are transferred to the prepreg and/or composite during processing. The presence of oils in the part could lead to problems in both mechanical and electrical performance of the part. This also guards against dermatitis that may occur with some users.; NONMETALLIC HONEYCOMB AND FOAM CORE USE: When using nonmetallic honeycomb and foam core materials for sandwich structures, the materials should always be dried in an oven prior to lay-up to drive off any moisture that may be in the core. The core should be cooled in the presence of a desiccant to avoid moisture uptake. Following drying, it is always best to use the material as soon as possible. Recommended core dry time/temp: 121°C (250°F) for 3–4 hours.; DEBULK LAY-UP MATERIAL SEQUENCE FROM TOOL SURFACE TO BAGGING MATERIALS:; A debulking procedure was necessary to minimize entrapped air between plies as shown in Figure 1. Pulled vacuum was at least at 27 inHg. TC350-1 prepreg layers were debulked at ambient every 4 plies for 5–10 minutes. An additional ply of porous Teflon coated glass (TX1040) was used to help the removal of entrapped air and it was replaced after being used for 2–3 times of debulking.

Show in full

Material Features

• Good Balance of Properties
• Good Mechanical Properties
• Low Water Absorption

HIGHLIGHTS

Robust under vacuum bag only (VBO) processing (very low void content); Excellent mechanical property translation; High toughness; Easy processing; Excellent tack properties; Good surfacing properties

Recommended Applications

• Launch
• Aerostructures
• Space structures
• Radomes and antennas
• Reflectors

Composite Materials Functions

Prepreg

Composites Processing Methods

• Compression Molding
• Out of Autoclave Prepreg
• Vacuum Bagging