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Renegade Materials Corporation RM-2005

Renegade Materials Corporation RM-2005 is a 350°F Curing Toughened Epoxy Prepreg system. In response to widespread aerospace market demand for an alternative to industry-standard toughened epoxies, has developed the NEXT generation Toughened Epoxy Prepreg, optimized for both hand-lay-up and automated fiber placement (AFP) processing. RM-2005 is supported by an extensive mechanical property database on both carbon tape and fabric. Excellent mechanical performance and damage tolerance makes RM-2005 a superior choice for military or commercial structural applications. RM-2005 is readily available with no minimum order quantities and the fastest lead times in the industry.

Polymer Name: Epoxy Resins & Compounds

Functions: Prepreg

Reinforcement Material: Carbon Fibers, Glass Fibers

Processing Methods: Vacuum Bagging

Technical Data Sheet
  • TypeDocument Name
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Knowde Enhanced TDS

Identification & Functionality

Chemical Family

Epoxy & Epoxy Derivatives

Polymer Name

Epoxy Resins & Compounds

Reinforcement Material

Carbon Fibers,

Glass Fibers

Composite Materials Functions

Prepreg

Technologies

Composite Materials

Product Families

Composite Materials — Prepregs & Molding Compounds

Thermoset Prepregs

Features & Benefits

Materials Features

Cost Effective,

Drapability,

Ease of Handling,

Excellent Toughness,

Good Compressive Strength,

Good Electrical Properties,

Good Mechanical Properties,

Low Dielectric Constant

Features
  • Typical RM-XXXX Resin Properties
  • Straightforward 350°F Cure.
  • Designed for demanding aerospace structural applications.
  • Developed for optimized tack and handle ability.
  • Delivers an excellent balance of properties for service up to 300oF.
  • Available in woven, unidirectional and slit-tape product forms using all fibers including carbon, quartz and glass.
  • Nano-enhancements for tailored laminate properties and multi-functional performance available.

Applications & Uses

Markets

Automotive & Transportation

Applications

Automotive & Transportation — Transportation

Aerospace & Aviation

Composites Processing Methods

Vacuum Bagging

Recommended cure cycle

All temperatures and times are based upon the lagging thermocouple unless otherwise specified.
Step 1. Vacuum hold for 60 minutes at room temperature
Step 2. Heat 1 – 10°F/ minute to 350 ± 10°F apply 30 ± 5 psig pressure until temperature reaches 225 ± 5°F
Step 3. Apply 85 ± 5 psig autoclave pressure and vent to atmosphere.
Step 4 Hold temperature at 350 ± 10°F for 120 +15/ -0 minutes.
Step 5. Cool at 1 – 10°F/ min, when temperature is below 150°F release pressure.

Properties

Physical Form

Prepreg

Technical Details & Test Data

Glass Transition Temperature Data

Renegade Materials Corporation RM-2005 - Glass Transition Temperature Data

Viscosity Profile

Renegade Materials Corporation RM-2005 - Viscosity Profile

Bagging Scheme

Renegade Materials Corporation RM-2005 - Bagging Scheme