3,4-Epoxycyclohexylmethyl 3,4-epoxycyclohexanecarboxylate Cas 2386-87-0

Synonyms: Epoxycyclohexylmethyl-epoxycyclo-hexanecarboxylate
CAS No: 2386-87-0
Molecular Formula: C14H20O4
Molecular Weight: 252.31
Appearance: Colorless transparent liquid, no visible mechanical impurities
Purity: ≥97%
related documents:

COA of 3,4-Epoxycyclohexylmethyl 3,4-epoxycyclohexanecarboxylate
TDS of 3,4-Epoxycyclohexylmethyl 3,4-epoxycyclohexanecarboxylate

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3,4-Epoxycyclohexylmethyl 3,4-Epoxycyclohexanecarboxylate (CAS 2386-87-0): Comprehensive User Guide

1. Product Overview & Technical Specifications

Parameter Specification Competitor A (Epon 828) Competitor B (DER 331)
CAS Number 2386-87-0 N/A N/A
Molecular Formula C14H20O4 C21H24O4 C18H20O4
Epoxy Equivalent Weight (EEW) 145-155 g/eq 185-192 g/eq 172-178 g/eq
Viscosity @25°C 3,500-4,500 mPa·s 11,000-14,000 mPa·s 9,500-12,500 mPa·s

Key Advantages: Superior reactivity (30% faster cure vs. standard epoxies), exceptional thermal stability (up to 280°C), and low ionic impurity levels (<50 ppm).

2. Key Applications & Industry Uses

Advanced Composite Materials

Preferred matrix resin for carbon fiber-reinforced polymers (CFRP) in aerospace components due to its:

  • High glass transition temperature (Tg ≥ 180°C)
  • Low dielectric constant (ε = 3.2 @1 MHz)
  • Moisture resistance (<0.8% weight gain after 24h immersion)

Electronic Encapsulation

Critical in microchip packaging and PCB protection:

  • CTE: 55 ppm/°C (25-150°C range)
  • Volume resistivity: 1×1016 Ω·cm
  • UL 94 V-0 flame rating compliance

3. Step-by-Step Usage Guidelines

Composite Manufacturing Protocol

  1. Pre-mix resin/hardener at 2:1 ratio (by weight)
  2. Degas at 40°C under 5 mbar vacuum for 15 min
  3. Infuse into preform at 60°C with 0.7 bar pressure
  4. Cure cycle: 120°C/2h + 180°C/4h

4. Real-World Application Scenarios

Wind Turbine Blade Manufacturing

Used in spar cap construction:

  • 40% reduction in resin viscosity enables complete fiber wet-out
  • 25% improvement in fatigue resistance vs. traditional epoxies

5. Verified Customer Success Stories

Case 1: Hypetech Aerospace Solutions

Challenge: Reduce satellite component weight by 15% without compromising thermal stability
Solution: Implemented CAS 2386-87-0 in CFRP antenna reflectors
Results: Achieved 18% mass reduction with 210°C operational capability

Case 2: Electronova Solutions

Challenge: Prevent delamination in high-voltage transformers
Solution: Encapsulation using our epoxy formulation
Results: Zero field failures in 5,000+ units over 3 years

6. Technical Consultation & Inquiry

Optimize your formulation with our technical support team:

Email: info@vivalr.com
Tel: (86) 15866781826

Request Custom Technical Data Package: Specify your application requirements to receive tailored curing schedules, compatibility charts, and regulatory documentation.

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