Bismaleimide Resin Powder (4,4'-BMI, High-Temperature Monomer)

CAS 13676-54-5In StockSample available

Key Features

  • Tg 280-320°C — highest Tg in processable addition thermoset family
  • Addition polymerization — no volatile byproducts during cure
  • Processable in standard 177°C autoclave infrastructure
  • Excellent high-temperature strength retention (>200°C service)
  • Standard monomer for BMI/DDM and BMI/epoxy toughened systems

Bismaleimide Resin (4,4'-bismaleimidodiphenylmethane, BMI, CAS 13676-54-5) is the standard difunctional BMI monomer for high-temperature thermoset applications. The maleimide groups polymerize via addition mechanism at 150-200°C without releasing volatile byproducts, yielding a highly cross-linked aromatic imide network with Tg of 280-320°C — significantly higher than the best epoxy systems (Tg <230°C).

Pure BMI monomer is a yellow crystalline powder (melting point 155-160°C) that melt-processes or dissolves in solvents (DMF, NMP, acetone) for prepreg and solution impregnation. The neat resin is brittle (KIc ~0.5 MPa·m0.5) and requires toughening through co-reactants: (1) diaminodiphenylmethane (DDM): classic toughening co-monomer at 30-40% by weight — reacts with BMI at 150-160°C to extend chain; (2) epoxy novolac (epoxy-novolac-f44): hybrid BMI/epoxy blends at 20-40% epoxy improve toughness while sacrificing some Tg; (3) allylphenyl compounds (DABA, eugenol): reactive tougheners via Diels-Alder mechanism.

BMI is the choice when epoxy maximum Tg (200-230°C) is insufficient for the application: aerospace engine structures above 200°C, military aircraft high-temperature zones, primary structural elements in supersonic aircraft, and radar-transparent composites requiring high-temperature stability. BMI composites are processable in standard 177°C autoclave infrastructure — unlike polyimide (PMR-15) which requires >300°C processing.

Specifications

ParameterValue
Purity>99%
AppearanceYellow crystalline powder
Melting Point155-160°C
Processing FormMelt (>160°C) or solution (DMF, acetone)
Cure Temperature150-200°C + post-cure 230-250°C
KIc (neat, cured)~0.5 MPa·m⁰·⁵
Tg (cured, with DDM)280-320°C

Applications

High-temperature aerospace composite structures (>230°C service)Military aircraft primary structure (supersonic zones)Jet engine component composites (nacelles, thrust reversers)Radar-transparent composite radomes (high-temperature stability)BMI/epoxy hybrid prepreg systems

FAQ

BMI/DDM (4,4'-bismaleimidodiphenylmethane + 4,4'-diaminodiphenylmethane) is the classic toughened BMI formulation, developed in the 1970s and still used in major aerospace programs. The Michael addition of DDM primary amine to BMI maleimide double bond extends the chain at 130-150°C before the maleimide homopolymerization crosslinking at 175-200°C. Standard ratio: 100g BMI + 30-35g DDM (by weight). This formulation achieves Tg 280-300°C with significantly improved toughness (KIc 0.8-1.2 MPa·m0.5) versus neat BMI (KIc 0.5 MPa·m0.5). Cure schedule: 150°C/2h + 177°C/2h + 230°C/2h post-cure. BMI/DDM prepregs are the matrix resin in Cytec 5250-4, Hexion CYCOM 5250-4-RTM, and similar commercial aerospace BMI systems.

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