CYTEC Engineered Materials > Composite Prepregs > Selector Guide

Select a CYTEC Composite Prepreg Product:
 
Primary Structures | Secondary Structures | High Temperature Materials | Interior Products | Thermoplastics | Carbon Friction Materials | Automotive Prepregs | Surfacing | Automotive Adhesives | Surfacing Films | Composite Tooling | Space Composites | Ballistic Applications | Sporting Goods | Space Adhesives | Marine Applications | Cure Adhesives | Dual Cure Adhesives | Ablatives | High Temperature Adhesives | Foam Adhesives | Aerospace Adhesives | Core Splice Adhesives | Epoxies, Pastes & Fillers | Potting Compounds | Resin Infusion Materials | Silicone Coatings | Silicone Castables | Silicone Firewall Sealants | Silicone Rubber | Complimentary Products

 

Composite Prepregs — Primary Structures

Resin Resin Type Recommended Adhesive Cure Temp. Dry Tg Wet Tg Current Representative Applications
CYCOM 997 Epoxy FM 355 350º 410 320 Nacelles, engine components, fairings
CYCOM 5250-4 BMI MB 2550 350º 565 410 Engine components, wing skins, high temperature components, industry standard high temperature primary structure material
CYCOM 5270-1 BMI MB 2550 350º 560 440 Engine components, high temperature components
CYCOM 977-2 Epoxy FM 300 350º 390 285 Tape-placed fuselage, high CAI driven components
CYCOM 977-3 Epoxy FM 300, FM 300-2 for core bonding 350º 430 300 Wing skins, ribs, spars, medium CAI driven components
CYCOM 934 Epoxy FM 300, MB 1515-3, FM 377 also used at Wichita 350º 380 320 Vanes, engine components, nacelles, 1st generation epoxy
CYCOM 5276-1 Epoxy FM 300-2 300º 380 300 Ultra high CAI, >45Ksi, helicopter components, sidewalls
CYCOM E 767 Epoxy FM 355 350º 400 305 Nacelles, thrust reversers
CYCOM E 773 Epoxy MB 1113, FM 94 250º 310 240 Rotor blades, spars
CYCOM 5216 Epoxy MB 1113, FM 94 250º 285 190 Rotor blades, spars
CYCOM 950-1 Epoxy FM 94, FM 300-2 260º 350 290 Rotor components, fuselage, wing structures

 

Composite Prepregs — Secondary Structures and Flight Control Surfaces

Resin Resin Type Recommended Adhesive Cure Temp. Dry Tg Wet Tg Applications
CYCOM 7701 Epoxy FM 123-2, FM 94 250º 260 190 Flaps, ailerons, fairings, radomes
CYCOM 7714 Epoxy FM 123-2, FM 94 250º 260 190 Mainly Aramid secondary structures
CYCOM 7740 Epoxy FM 94, FM 300-2 250º 250 205 Engine acoustic treatments, exterior aircraft components
CYCOM 7668 Epoxy FM 355 350º 400 320 Sandwich structures, high temperature ducting
CYCOM 970 Epoxy MB 1515-3, MB 1515-4 350º -- -- Control surfaces, core structures
CYCOM 919 Epoxy FM 123-2, FM 94 250º 290 220 Ducting, fairings, interior components
CYCOM 4102 Polyester FM 4102SP,
developed as surface ply only		 250º 250 -- Interior components
CYCOM 5208 Epoxy FM 300, MB 1515-3 350º 410 290 Control surfaces, radomes, nacelle components

 

 

 

 

 

 

 

Composite Prepregs — High-Temperature Materials

Resin Type Features and Benefits Typical Applications Minimum
C ure Temp.
ºF/ºC		 Toughness
(1)		 Tg (2)
ºF/ºC
Dry		 Out Life
at 77ºF/
25ºC
AVIMID K3B Condensation polyimide Thermoplastic polyimide which is reprocessable. Outstanding compression after impact (CAI) damage tolerance with 55 ksi (379 MPa). Better thermo-oxidative stability (TOS) and more microcrack resistant than PMR-15. Primary and secondary aircraft structures. High temperature aircraft components. 640/338 High 473/245 10 days
AVIMID N Condensation polyimide Highest thermo-oxidative stability (TOS) of the three AVIMID® resins. Low dielectric constant for radome applications. High toughness. Compression moldable. More microcrack resistant than PMR-15. Primary and secondary aircraft structures. Engine components. 640/338 High 644/340 10 days
AVIMID R Condensation polyimide Excellent compression after impact (CAI) damage tolerance with 40 ksi (276 MPa). High thermo-oxidative stability (TOX). More microcrack resistant than PMR-15. Compression moldable. Primary and secondary aircraft structures. Engine components. 640/338 High 590/310 10 days
AVIMID RB Polyimide A high temperature, Tg 644ºF/340ºC, thermoset polyimide resin with wet service capability to more than 530ºF/277ºC wet and 600ºF/316ºC dry service capability. AVIMID® RB has excellent thermal-oxidative stability and resistance to aircraft fluids. Specified for jet engine use. 680/360 -- 644ºF/340ºC 14 days
CYCOM 944 Condensation polyimide High strength and dimensional stabilitiy at elevated temperatures. Capable of vacuum bag processing. High temperature aerospace structures. 350/177 Low 630/332 4 weeks
CYCOM 2237 Polyimide (PMR-15) Industry standard high-temperature material. High strength and dimensional stability at elevated temperatures. Moderate thermo-oxidative stability (TOS) and microcrack resistant. Engine components. High temperature aircraft components. 600/316 Low 640/338 1 week
CYCOM 3002 Condensation polyimide High strength and dimensional stability at elevated temperature. MDA free system. Capable of vacuum bag processing. High temperature aircraft components. 350/177 Low 716/380 3 weeks/
no tack
CYCOM 3010 Fully imidized PMR-15 MDA free, this PMR-15 based material is delivered in fully imidized form, it can be processed using conventional high-temperature methods. Capable of vacuum bag processing. Engine components. High temperature aircraft components. 600/316 Low 640/338 1 year
CYCOM 5004 Condensation polyimide High strength and dimensional stability at elevated temperatures. Self-extinguishing and low smoke generation. High temperature insulation and circuit boards. 350/177 Low 630/332 4 weeks
CYCOM 5245C Modified cynate ester Excellent mechanical properties. Good hot/wet performance. Excellent dielectric properties. Post cure is required. Primary aircraft structures, radomes and space systems. 350/177 Medium 420/216 3 weeks
CYCOM 5250-2 Modified BMI Excellent balance of mechanical properties and high temperatures. Post cure is required. Primary and secondary aircraft structures. Engine components. 350/177 Low 565/296 4 weeks
CYCOM 5250-4

CYCOM 5250-4 RTM 		Modified BMI Industry leading BMI material. Excellent toughness and mechanical performance. Noted for hot/wet performance up to 350ºF/177ºC, has 15% better RTA properties than any epoxy resin system. Post cure is required. Primary and secondary aircraft structures. F-22 wing and fuselage. Thrust reversers and other high temperature aircraft and helicopeter components. 350/177 Medium 565/296 4 weeks
CYCOM 5260-2 Modified BMI Outstanding toughness. Mechanical properties of 5250-4 with 45 ksi (310 MPa) compression after impact (CAI) values. Controlled flow. Post cure is required. Primary aircraft structures requiring high level of damage tolerance. 350/177 High 550/288 4 weeks
CYCOM 5270 Modified BMI Designed for continuous use up to 450ºF/232ºC. Excellent mechanical properties and thermal stability approaching PMR-15. Post cure is required. Engine components. High temperature aircraft components. 350/177 Low 562/294 2 weeks
CYCOM 5575 Modified cynate ester Designed for radomes and low observable structures, low dielectric and loss tangent. Excellent hot/wet performance. Low moisture uptake, low out-gassing. Complete line of adhesives and syntactic materials available based on 5575 chemistry. Radomes and antennas. Space applications. 350/177 Medium 450/232 3 weeks

 

Composite Prepregs — Interior Products

Resin Resin Type Recommended Adhesive Cure Temperature Dry Tg

Applications
CYCOM 6070 Phenolic NA 280º 500 Crush core and MOP process, sidewalls, stowbins — BMS 8-222, 274 qualified
CYCOM 2265 Phenolic NA 280º 400 Crush core, vacuum bag and MOP process, sidewalls, stowbins — BMS 8-226 qualified
CYCOM 2290 Phenolic NA 280º 400 Crush core, vacuum bag and MOP process, sidewalls, stowbins — BMS 8-226 qualified
CYCOM 2400 Phenolic NA 280º 400 Sidewalls and stowbins
CYCOM 6825-1 Phenolic -- 250º 400 Next generation phenolic — low smoke and toxicity
CYCOM 6826 Phenolic NA 260º 400 Self-adhesive to core
CYCOM 6001 Phenolic HT 424 or
HT 435		 320º 500 Good ablative properties

 

 

 

 

 

 

 

 

Composite Prepregs — Thermoplastics

Thermoplastic Features and Applications Min. Consolidation Temp. ºF/ºC Service Temp. ºF/ºC Toughness (1)
APC-2 PEEK (poly-ether-ether-ketone) based thermoplastic with high temperature and mechanical performance. Excellent environmental resistance, very low flame and smoke, high toughness and fatigue resistance, low wear. May be used in stamping and tape laying/wrapping. Applications include aircraft primary structures, space components, and wear resistant applications. May be used at temperatures above Tg due to the crystallinity of polymer. 720/382 250/121 (aerospace) 500/260 (non- aerospace) High
APC (PEKK) High toughness and excellent chemical resistance. Very low flammability, smoke and toxicity. Used in aircraft interiors, aerospace structure and industrial applications. 640/338 250/121 High
APC (PEI) High toughness with good chemical resistance. Low flammability, smoke and toxicity. Standard grade not recommended for use in hot hydraulic fluids. Improved environmental resistance grade available. Applications include aircraft interiors and high performance industrial applications. 600/315 300/150 High
APC (PPS) Excellent chemical resistance. May be used at temperatures above Tg due to the crystallinity of the polymer. Applications include aerospace and high performance engineering applications. 600/315 150/65 (aerospace) 400/204 (non-
aerospace) 		Medium
CYCOM 5303 Modified PES polymer with lower temperature processability. Application includes cargo liners and aircraft interiors. Low heat release and smoke evolution. 350/177 300/149 High
CYCOM 5305 CYCOM 5303 with a proprietary flame retardant. Intended for use as fire barrier. 350/177 300/149 High
CYCOM 5315 Modified PEI polymer with low temperature processability. Application includes aircraft interiors. Flame retarded, low smoke, low flammability. 350/177 300/149 High

Thermoplastic Sheet
Thermoplastic Sheet Features and Benefits Forming Temp.
ºF/ºC 		O.S.U. (2) QP/QT Vertical Burn Length (3) in. (cm)
DECLAR Thermoplastic sheet without PVF film that meets fire, smoke and toxicity requirements for aircraft interiors. 370 to 430/ 188 to 221 <40/<20 2.5 (6.35)
DECLAR T Thermoplastic film laminated with PVF film which improves the durability and photo-stability. It's easier to clean and eliminates secondary operation. 370 to 410/ 188 to 210 <55/<30 2.5 (6.35)
DECLAR T-SP Thermoplastic film laminated with PVF SP grade with similar features as DECLAR T. DECLAR T-SP offers the added advantage of matching low gloss, wide color ranges typically used in aircraft interior parts. 370 to 410/ 188 to 210 <55/<30 2.5 (6.35)

Avimid High-Temperature Thermoplastics

Thermoplastic

 Type Features and Benefits Typical Applications Minimum Cure Temp ºF/ºC Toughness (1) Tg (2) ºF/ºC  Dry
 Out Life at 77ºF/25ºC
AVIMID K3B Condensation polyimide

Thermoplastic polyimide which is reprocessable. Outstanding compression after impact (CAI) damage tolerance with 55 ksi (379 MPa). Better thermo-oxidative stability (TOS) and more microcrack resistant than PMR-15.

Primary and secondary aircraft structures. High temperature aircraft components. 640/338 High 473/245 10 days

Notes:

  • Interior thermoforming sheets: Cytec Engineered Materials offers aesthetically appealing thermoforming sheets for producing interior parts such as decorative laminates, stowage bins, window panels, partition galleys, seat backs, lavatories and moldings. DECLAR® thermoplastic sheets are offered in a variety of thicknesses, colors and textures. All products can be used with existing thermoforming equipment.

Cytec Engineered Materials has developed a range of high-performance thermoplastic composites to complement our extensive range of thermosetting composites. Our thermoplastic product forms include blends of commingled polymer and reinforcements, uni-direction fibers and woven fabrics. The full impregnated forms can be processed by rapid forming such as stamping and in-situ tape placement. Typical processing includes press forming, stamping, tape/tow placement and autoautoclave consolidation. A feature of all the thermoplastic materials is that they may be reprocessed and formed multiple times. All of our prepreg products can be processed through the use of autoautoclaves, press and vacuum bag/oven.

  1. Toughness - Compression after impact (CAI) 1500 in-lbs/in laminate thickness performed  on a 4" x 6", 24 to 32 ply quasi-isotropic laminate. Low = Below 28 ksi (193 MPa); Medium = 28 to 37 ksi (193 to 255 MPa); High = 37 ksi (255 MPa) and above.
  2. OSU tested to FAR 25.853 Appendix F. AP(kW/m2) = Peak heat released. QT (kW*min/m2) = Total heat released.
  3. Burn length based on 60 seconds exposure to a Bunsen burner.

 

Carbon Friction Materials

Resin

 Form Description Features and Benefits Advantages Processing Method
KARBON 415 Chopped tow molding compound. One step phenolic resin system reinforced with carbonized PAN fiber. Molds to near-net-shape. Typically converted to carbon-carbon for aircraft or atutomotive brakes. Proven in numerous applications. Easily formed into complex shapes. Capable of high fiber volume content. Compression mold.
KARBON 616 Chopped tow molding compound. One step phenolic resin system reinforced with carbonized intermediate modulus pitch fiber. Molds to near-net-shape and offers a higher achievable density. Typically converted to carbon-carbon for aircraft or motive brakes. Same as above. Compression mold.
KARBON 641 Broadgood or bias tape One step phenolic resin system reinforced with heat stabilized 8HS PAN fabric. Typically converted to carbon-carbon for use in high temperature, leading edge applications. Proven in numerous applications. Envolute or tape wrap autoclave/ hydroautoclave.
KARBON 663 Chopped tow molding compound. One step phenolic resin system reinforced with carbonized high modulus pitch fiber. Molds to near-net-shape and offers higher thermal conductivity. Typically converted to carbon-carbon for aircraft brakes. Same as above. Compression mold.
FM 5064W Broadgood or bias tape. One step phenolic resin system reinforced with graphitized rayon fabric. Typically converted into 2D carbon-carbon components. Resin matrix allows high temperature processing without delamination. Envolute or tape wrap autoclave/ hydroautoclave.
KARBON Preform Near-net-shape substrate. Woven or non-woven preforms with engineered or random fiber orientation. Available in a wide selection of fibers and textile architectures. Textile technology offers improved mechanical strength and customizable properties for higher performance. Typically converted to carbon-carbon for demanding friction applications and high thermal conductivity products. Enhanced homogeneity. Eliminates consolidation steps. Provides a manageable part. When resin-free, no carbonization required. Ready for carbon-carbon densification process.

 

Automotive Prepregs

Prepreg Features and Applications Minimum Recommended Processing Condition Toughness (1) Service Temp. Dry ºF/ºC Out Life at 77ºF/25ºC
CYCOM 2020 A versatile curing, modified epoxy-based prepreg system which can be cured from 80ºC to 180ºC depending on desired service temperature. CYCOM® 2020 has an out-life in excess of 4 weeks at ambient conditions and maintains good drape and tack characteristics throughout. Displays excellent rentention of mechanical performance at elevated temperatures. 10 hrs. at 175ºF/80ºC + optional 1 hr. at 275ºF/135ºC post cure High -- 8 weeks
CYCOM 759 Modified epoxy prepreg. Provides superb surface finish with good hot/wet performance. 14 hrs. at 160ºF/70ºC Medium 195/91 4 weeks
CYCOM 761 Modified epoxy prepreg. Designed for use as thermal barriers (non load bearing) in motor sport applications. The short term maximum service (operational) temperature is 572ºF/300ºC, which exceeds most epoxy prepreg. Quick processing cycles. Post cure at 390ºF/199ºC is required. 4 hrs. at 175ºF/79ºC or 45 min. at 250ºF/121ºC Low 414/212 2 weeks
CYCOM 919CYCOM 919 LB
CYCOM 919 HF 		Modified epoxy prepreg. 919 is widely recognized as the industry standard in race car construction. High toughness with mechanical performance and flame retardant. Self-adhesive with 4 weeks tack life, suitable for sandwich panel construction. Also available in high flow version. 1.5 hrs. at 250ºF/121ºC Medium 290/143 4 weeks
CYCOM 950-1 Modified epoxy prepreg. A 250ºF/121ºC curing system with the performance of a 350ºF/177ºC curing epoxy. A toughened system exhibiting excellent mechanical properties. 2 hrs. at 260ºF/127ºC Medium 350/177 4 weeks
CYCOM 985 Modified epoxy prepreg. Suitable for the manufacture of carbon composite block for use in machining of solid carbon inserts. 2 hrs. at 350ºF/177ºC Low 379/193 10 days
CYCOM 977-2 Modified epoxy prepreg. Excellent hot/wet properties. Controlled flow, good surface characterics. 3 hrs. at 350ºF/177ºC High 392/200 10 days
CYCOM 977-6 Modified epoxy prepreg. Excellent hot/wet properties. Also used for primary aircraft structures. 2 hrs. at 310ºF/154ºC High 356/180 10 days
CYCOM 5215 Modified epoxy prepreg. Curable at 150ºF/66ºC with only vacuum bag pressure. The cured part will yield less than 1% void content. Mechanical property and service temperature range equivalent to 1st generation epoxy prepreg after post cure at 350ºF/177ºC. Prototyping, repair, tooling and structural application where controlled cost processing is desired. 14 hrs. at 150ºF/66ºC + 2 hrs. at 350ºF/177ºC post cure Low 375/191 10 days
CYCOM 5250-4 Modified bismaleimide prepreg. Aerospace industry standard BMI. 5250-4 has toughness equal to the best toughened epoxy prepregs combined with controlled degradation in mechanical performance up to 375ºF/191ºC. Used for components or structures where thermal performance requirements exceeds the capability of epoxies. Outstanding mechanical properties throughout its temperature range. 6 hrs. at 350ºF/177ºC Medium 565/296 4 weeks
CYCOM 5276-1 Modified epoxy prepreg. Ultra tough epoxy with excellent hot/wet mechanical properties. Industry leading damage tolerance, Compression After Impact (CAI) consistently above 45 ksi (310 MPa). Controlled flow, excellent handling and tack. Can be cured at 300ºF/149ºC. 2 hrs. at 300ºF/149ºC High 380/193 2 weeks
CYCOM 7740 Modified epoxy prpreg. Flame retardant material, good high temperature properties and thermal stability. 180ºF/82ºC wet service temperature. 2 hrs. at 250ºF/121ºC Low 250/121 2 weeks
CYCOM 97714A Modified epoxy prepreg. Self extinguishing, high structural properties in solid laminates.Self-adhesive to honeycomb core. Good flatwise tensile strength. Controlled flow and vacuum bag processable. 2 hrs. at 250ºF/121ºC Low 260/127 10 days

Notes: All of our prepregs can be processed through the use of autoclaves, press and vacuum bag/oven.

  1. Toughness - Compression After Impact (CAI) 1500 in-lbs/in laminate thickness performed on a 4" x 6", 24 to 32 ply quasi-isotropic laminate. Low=Below 28 ksi (MPa); Medium=28 to 37 ksi (193 MPa); High=37 ksi (255 MPa) and above.
  2. Service (operational) temperature is typically 50ºF below the glass transition temperature (Tg). Service temperature is also dependent on the stresses the structure is exposed to.

 

Automotive Adhesives

Prepreg Features and Applications Minimum Recommended Processing Condition Service Temp. Dry ºF/ºC
FM 73 Modified epoxy film adhesive. Industry standard toughened adhesive. Proven in metal-metal, composite-composite bonding. 1 hr. at 250ºF/121ºC 180/82
FM 87-1HT Modified epoxy film adhesive. Excellent composite-composite and metal-metal bonding with ideal handling characteristics. 1 hr. at 250ºF/121ºC 250/121
BR 95 Two-part modified epoxy past adhesive. Good composite-composite and metal-metal bonding. Flexible cure profile. 5 days at 75ºF/24ºC or 1 hr. at 200ºF/93ºC 300/149
FM 300-2 Modified epoxy film adhesive. A flexible cure version of FM 300. Excellent co-cure and co-bond strength under a wide variety of bonding conditions. Can be cured over the range of 250 to 300ºF/121 to 149ºC with no change in properties. 1 hr. at 250ºF/121ºC 300/149
BR 623 Modified epoxy potting compound. Low density, 1 component potting compound for core reinforcement for hard point attachment and edge fill. Its unique, "soft butter" texture promotes ease of use and void-free construction. 1 hr. at 250ºF/121ºC 200/93
FM 755 Modified epoxy adhesive. Co-curable with CYCOM 752-2. Variable cure up to 275ºF/135ºC. 14 hrs. at 160ºF/70ºC 160/71

 

Adhesive Surfacing Films

Product Description Standard Weight Cure Temperature Tg Vacuum Bag Cure?
SURFACE MASTER 202 Next generation surfacing film used primarily in high-perfomance motive industry; provides smooth surface requiring minimum preparation for painting. Co-curable with composite matrix resins at 250-350ºF (121-177ºC). Minimizes honeycomb core mark-through, porosity and core crush. Excellent tack and drapability, with shop life of greater than 30 days ambient. .035/.060/
.080 psf 		250-350ºF/
121-177ºC		 298 No
SURFACE MASTER 905 Next generation surfacing film; offers increase in surface quality, virtually eliminating sweep and fill operations, as well as potentially eliminating paint primer operations. Offers increase in shop lifetime (45 days), drastically reduces residue left on tool, and has excellent tack and drape characteristics at room temperature. Compatible with most 250-350ºF (121-177ºC) autoclave or vacuum bag cure systems. .035/.045 psf 250-350ºF/ 121-177ºC 298 Yes
SURFACE MASTER 905C Clear version of Surface Master 905. The clear version is designed to provide transparency for applications where it is important to be able to see the prepreg under the surfacing film. Surface Master 905C has excellent tack and handling properties and is designed to provide porosity-free surface when co-cured with most 250ºF and 350ºF curing epoxy based prepreg systems. .035 psf 250-350ºF/ 121-177ºC 298 Yes
FM 300 1st generation surfacing film; superior metal-to-metal peel strength, composite-to-composite bonding, and composite-to-metal joints. Extensively used as surfacing ply for composite materials. .030 psf 350ºF/
177ºC		 296/147 No
FM 300-2 1st generation surfacing film; 250ºF (120ºC) cure version of FM 300. In addition, has a processing window including temperatures up to 300ºF (150ºC) providing a unique level of flexibility from one adhesive product. Developed specifically for co-cure and secondary composite bonding applications. .030 psf 250-350ºF/ 121-177ºC 290/145 No
FM 1515-3 1st generation surfacing film; industry standard for composite bonding and surfacing applications. Designed for co-cured, pre-cured and co-bonding of composite materials. .030 psf 350ºF/
177ºC		 300/149 No

 

Adhesive Materials — Surfacing Films

Product Description Standard Weight Cure Temperature Tg Vacuum Bag Cure?
SURFACE MASTER 202 Next generation surfacing film used primarily in high-perfomance motive industry; provides smooth surface requiring minimum preparation for painting. Co-curable with composite matrix resins at 250-350ºF (121-177ºC). Minimizes honeycomb core mark-through, porosity and core crush. Excellent tack and drapability, with shop life of greater than 30 days ambient. .035/.060/
.080 psf 		250-350ºF/
121-177ºC		 298 No
SURFACE MASTER 905 Next generation surfacing film; offers increase in surface quality, virtually eliminating sweep and fill operations, as well as potentially eliminating paint primer operations. Offers increase in shop lifetime (45 days), drastically reduces residue left on tool, and has excellent tack and drape characteristics at room temperature. Compatible with most 250-350ºF (121-177ºC) autoclave or vacuum bag cure systems. .035/.045 psf 250-350ºF/ 121-177ºC 298 Yes
SURFACE MASTER 905C Clear version of Surface Master 905. The clear version is designed to provide transparency for applications where it is important to be able to see the prepreg under the surfacing film. Surface Master 905C has excellent tack and handling properties and is designed to provide porosity-free surface when co-cured with most 250ºF and 350ºF curing epoxy based prepreg systems. .035 psf 250-350ºF/ 121-177ºC 298 Yes
FM 300 1st generation surfacing film; superior metal-to-metal peel strength, composite-to-composite bonding, and composite-to-metal joints. Extensively used as surfacing ply for composite materials. .030 psf 350ºF/
177ºC		 296/147 No
FM 300-2 1st generation surfacing film; 250ºF (120ºC) cure version of FM 300. In addition, has a processing window including temperatures up to 300ºF (150ºC) providing a unique level of flexibility from one adhesive product. Developed specifically for co-cure and secondary composite bonding applications. .030 psf 250-350ºF/ 121-177ºC 290/145 No
FM 1515-3 1st generation surfacing film; industry standard for composite bonding and surfacing applications. Designed for co-cured, pre-cured and co-bonding of composite materials. .030 psf 350ºF/
177ºC		 300/149 No

 

Composite Tooling

Resin Cure Temperature
ºF 		Post Cure Temperature
ºF 		Service Temperature
ºF 		Out-life

Applications
CYFORM® 22 Ambient
72-250		 390 350 3 days Room temperature curing with low CTE and shrinkage
CYFORM 777 140-250 390 350 7 days Low CTE and shrinkage
CYCOM® 5215 150 350 325 10 days Vacuum-bag only technology
CYCOM 7620 150-250 375 350 -- --

Epoxy Ancillary Products
• CHP102 “Cytec Hard Paint”; high gloss master model sealing paint
• CGC108 surface gel coat
• CGC107-1 laminating resin
• SOLAM 5/6 boards; solid carbon or glass support laminates
• DAPCO® casting compounds
     – Trapped rubber molding; non-autoclave, reusable, no bag required, 10-20,000 psi pressure
     – Pressure intensifiers and caul pads for vacuum bag applications
• DAPCO 62 & 63 conformable/sprayable vacuum bags, repairable
• DAPCO 3400 coating; extends the life of reusable vacuum bags
• SMC silicone rubber
     – Cured for envelope bags (360º conformable molding) and debulking tables
     – Uncured (“B” stage) for conformal RVB construction
     – Extruded profiles for hat section stiffeners, inflatable mandrels, RVB seals and trapped rubber molding applications

BMI Tooling

Resin Cure Temperature
ºF 		Post Cure Temperature
ºF 		Service Temperature
ºF 		Out-life

Applications
DURATOOL® 450 350 440 450 25 days High cycles with no degradation
CYCOM 5270-1 350 450 450 -- Over 400ºF service

BMI Ancillary Products
• FM® 2550 & FM 2550B BMI film adhesive
• FM 475 syntactic core
• FM 6604-1 core splice adhesive
• BR® 450-4 potting compound

 

Space Composites

Resin Features and Benefits Typical Applications Minimum
Recommended
Cure Temp.
ºF/ºC 		Toughness
(1)		 Outgassing (2) Tg (3)
ºF/ºC Dry		 Out Life
at 77ºF/
25ºC
TWL% CVCM%
CYCOM 69-5 Modified epoxy prepreg. Co-curable with structural adhesives to produce thin skinned sandwich structures. Controlled flow. Aerospace and space approved. Antenna, bus structure, solar array, launch vehicles, R.L.V. 350/177 Low 0.67 0.01 397/203 2 weeks
CYCOM 934 Modified epoxy prepreg. Industry standard prepreg for space applications. Laminate and sandwich panel usage. Large database for aircraft applications. Launch vehicles, R.L.V. 350/177 Low 0.64 0.01 381/194 10 days
CYCOM 950-1 Modified epoxy prepreg. Controlled flow, vacuum bag cure capability. Aerospace and space approved. Antenna, bus structure. Solar array, space station, launch vehicles, R.L.V. 260/125 Medium 0.75 0.02 350/177 4 weeks
CYCOM 977-2 Modified epoxy prepreg. Controlled flow, high toughness. Aerospace, space approved. Launch vehicles, R.L.V., space station. 350/177 High N/A N/A 392/200 10 days
CYCOM 977-3 Modified epoxy prepreg. Higher service themperature than 977-2 with excellent hot/wet properties. Aerospace and space approved. Launch vehicles, R.L.V., space station. 350/177 Low N/A N/A 428/220 2 weeks
CYCOM 977-6 Modified epoxy prepreg. Excellent hot/wet properties. Launch vehicles, R.L.V., space station. 310/154 High N/A N/A 390/180 10 days
CYCOM 5276-1S Modified epoxy prepreg. Ultra tough, controlled flow. Industry leading damage tolerance, Compression After Impact (CAI) consistently above 35 ksi (241 MPa). Excellent handling and tack. Antenna, bus structure, solar array, space station, R.L.V. 300/149 Medium 0.71 0.01 380/193 2 weeks
CYCOM 5575-1S Modified cynate ester prepreg. Controlled flow, low moisture absorption. Good tack and drape. Good toughness. Antenna, bus structures, solar array, space station, R.L.V. 350/177 Medium 0.11 0.00 410/210 3 weeks
CYCOM 5575-1 RTM -350ºF/175ºC cure cyanate ester resin for up to 350ºF/175ºC continuous service, and particularly targeted for space applications. Space structures, and other aerospace and industrial applications requiring very good moisture resistance. 350/177 -- 0.21 0.01 -- 14 days

NOTE: CYCOM 977 resin lines offer a range of toughness and hot/wet performance. These materials can be used for structural applications associated with the delivery of space structures.

All of our prepreg products can be processed through the use of autoclaves, press and vacuum bag cure.

  1. Toughness - Compression After Impact (CAI) 1500 in-lbs/in laminate thickness performed on a 4" x 6", 24 to 32 ply quasi-isotropic laminate. Low = Below 28 ksi (193 MPa); Medium = 28 to 37 ksi (193 to 255 MPa); High = 37 ksi (255 MPa) and above.
  2. Outgassing: TWL=Total Weight Loss. CVDM=Collected Volatile Condensable Matter. Tested to NASA 1142.
  3. Service (operational) temperature is typically 50ºF below the glass transistion temperature (Tg).

 

Ballistic Applications

Resin Features and Applications Min. Consolidation Temp. ºF/ºC Service Temp. Dry ºF/ºC Out Life at 77ºF/25ºC
CYCOM 2282 Kevlar reinforced materials. Offering superior ballistic performance in compliance with FAA mandated test methods. Used in military rotorcraft, available for commerical applications such as cockpit doors and bulkheads. Available in prepreg or panel form, custom lengths for retrofit use. --- 275/135 10 days
CYCOM 7034 Polyester prepreg. Good all around properties with rapid cure cycles for low pressure molding. Excellent ballistics performance. 15 min. at 300ºF/149ºC 160/71 4 weeks
CYCOM 794 PVB modified phenolic prepreg. Flame retardant with excellent toughness characteristics good for reducing trauma effects from ballistic impact. High pressure molding. 15 min. at 320ºF/160ºC 250/121 12 weeks
CYCOM 796 Phenolic prepreg. Provides good ballistic properties along with excellent fire retartant and high temperature performance. High pressure molding. 30 min. at 300ºF/149ºC 500/260 4 weeks
CYCOM 4102 Polyester prepreg. Flame-resistant system used extensively in the manufacture of thick ballistic armament, and in composite infantry fighting vehicles. 2 hrs. at 250ºF/121ºC 250/121 3 weeks
CYCOM 6001 Phenolic prepreg. Low flammability, high temperature endurance, used mostly in flat armor. Good ballistic performance. 1 hr. at 300ºF/149ºC 500/260s 2 weeks
CYCOM 6400 PVB modified phenolic prepreg. Used in spall liners and helmets. Low flammability. Qualified to Mil-L-62474, Mil-A-62473. 30 min. at 330ºF/166ºC 220/104 1 year
CYCOM 9002 Polyester prepreg, non-styrenated. Flame retardant, good for high temperature aircraft secondary structures. Used in flat armor, helmets, good combination of mechanical and ballistics properties. 2 hrs. at 275ºF/135ºC 250/121 2 weeks
CYCOM 9420 Vinyl ester prepreg, non-styrenated. Low flammability, self-extinguishing. Good tack and drape. 1.5 hrs. at 275ºF/135ºC 275/135 2 weeks

All of our prepregs can be processed through the use of autoclaves, press and vacuum bag/oven.

 

Industrial Materials — Sporting Goods Grade
250ºF/121ºC Range Cure Epoxy Prepregs

Resin Features and Benefits Typical Applications Min. Recommended Processing Conditions Relative Toughness Tg (1) ºF/ºC Dry Tg (1) ºF/ºC Wet Out Life at 77ºF/25ºC
CYCOM 919HF High flow version of 919 providing exceptional toughness and compressive properties. Lower resin content versions result in high specific rigidity in the molded tube. Fishing rods, high impact tubular designs and other sporting applications. 1.5 hrs. at 250ºF/121ºC High 290/143 219/104 4 weeks
CYCOM 737 Versatile resin system providing excellent surfact finish in the molded component. Fishing rods, high impact tubular designs and other sporting applications. 1 hr. at 250ºF/121ºC Medium 290/143 219/104 4 weeks
CYCOM 948A1 Versatile resin system that is processing capable from shrink film wrapping to autoclave curing. Ideally suited for tubular structure applications. Produces high quality finish. Fishing rods and other sporting goods applications. 1.5 hrs. at 250 to 300ºF/121 to 149ºC Low 250/121 160/71 4 weeks
CYCOM 949 Higher toughness than 948A1 and is also used for sporting goods. Flow controlled and processing capable from shrink film wrapping to autoclave curing. Tennis rackets, golf shafts and other sporting goods applications. 1.5 hrs. at 250 to 300ºF/121 to 149ºC High 257/125 140/60 2 weeks
CYCOM 950C Similar stiffness, damage tolerance and low flow but with shorter gel time than 949 for faster processing. Processing capable from shrink tape wrapping to autoclave curing. Self adhesive in sandwich applications. Fishing rods, tennis rackets, golf shafts and other sporting goods applications. 1.5 hrs. at 250 to 300ºF/121 to 149ºC High 300/149 240/116 10 days
CYCOM 5217 Designed for tubular structure applications requiring optimum interlaminar shear characteristics. Fishing rods, tennis rackets, golf shafts and x-ray cassettes. 1 hr. at 250ºF/121ºC Low 290/143 240/116 4 weeks
CYCOM 5228-1 Flow controlled, toughened (36 ksi [248MPa] CAI) modified epoxy designed for demanding tubular structure applications. The toughness adds to long term durability. Fishing rods, tennis rackets, golf shafts, sail boat masts and other sporting goods applications. 1 hr. at 250ºF/121ºC High 260/127 175/79 4 weeks
CYCOM 7409 Low tack, high flow. Avaliable in a range of colors. Works well in press cure and bladder cure applications. Skies, vaulting poles, parallel bars, wind surfing masts. 1 hr. at 250ºF/121ºC Low 260/127 230/110 (no tack) 12 weeks shelf life at R.T.

Notes:

All of our prepreg products can be processsed through the use of autoclaves, press and vacuum bag/oven.

(1) Service (operational) temperature is typcially 50ºF below the glass transition temperature (Tg). Service temperature is also dependent on the stresses the structure is exposed to.

 

Space Adhesvies

Film Adhesive Recommended Primer Description, Features and Benefits Minimum Recommended Cure Temp.
ºF/ºC 		Service Temp.
ºF/ºC		 Outgassing (1) Tg ºF/ºC
TWL % CVCM %
FM 73 BR 6747-1;
BR 127

Modified epoxy film. General prupose, toughened adhesive, proven in metal-metal and metallic sandwich structure. Selected in PABST program for primary structural bonding of aluminum.

250/121 180/82 0.78 0.00 203/95
FM 96 BR 6747-1;
BR 127

Modified epoxy film. Good for bonding metals and composites. Does not require refrigerated storage.

350/177 350/177 0.53 0.11 350/177
FM 300 BR 6747-1;
BR 127

Nitirle epoxy. Toughened 300ºF/149ºC service temperature proven in metal-to-metal, composite and sandwich structure. Excellent surfacing characteristics.

350/177 300/149 0.92 0.07 296/147
FM 300-2 BR 6747-1;
BR 127

Epoxy. 250ºF/121ºC cure version of FM 300. Recommended for both co-cured and secondary bonding of composite structure and for metal-metal bonding applications. Excellent surfacing characteristics.

250 to 350ºF/121 to 177ºC 300/149 0.97 0.08 290/143
HT 424 BR 424

Phenolic epoxy. Capable of withstanding short term exposure to 1,000ºF/538ºC. HT 435 adhesive (aluminum-free grade).

350/177 500/260 0.83 0.17 358/181
FM 1146-3 BR 6747-1;
BR 127

Epoxy. Provides excellent balance of peel strength and elevated temperature performance. Designed for metal-metal bonding, pre-cured and co-cured composite applications.

250 to 350ºF/121 to 177ºC 250/121 0.38 0.03 280/138

 

Marine Applications

Resin Features and Benefits Typical Applications Min. Recommended Processing Conditions Relative Toughness Tg (1) ºF/ºC
Dry		 Out Life at 77ºF/25ºC
CYCOM 754 Modified epoxy prepreg. Developed specifically for marine structures. Variable cure up to 250ºF/125ºC. Boat hulls, decks, etc.

10 hrs. at 160ºF/70ºC

Medium

195/91 3 weeks
CYCOM 753 Modified epoxy prepreg. Developed specifically for marine applications. Excellent balance of toughness and mechanical properties. Allows low cure temp.
 Boat hulls, decks and steering components.
 8 hrs. at 140ºF/60ºC


 Medium 190/88 1 week
CYCOM 950-1 Modified epoxy prepreg. A 250ºF/121ºC curing system with the performance of a 350ºF/177ºC curing epoxy. A toughened system exhibiting excellent mechanical properties. Masts and appendages. 2 hrs. at 260ºF/127ºC Medium 350/177 4 weeks
CYCOM 919HF Modified epoxy prepreg. A high flow version of CYCOM 919 providing exceptional toughness and compressive properties. Low resin content prepreg available, which results in high specific rigidity in molded structures. Masts and appendages. 1.5 hrs. at 250ºF/121ºC High 290/143 4 weeks
CYCOM 2020 A versatile curing, modified epoxy-based prepreg system which can be cured from 80ºC to 180ºC depending on desired service temperature. CYCOM 2020 has an out-life in excess of 4 weeks at ambient conditions and maintains good drape and tack characteristics throughout. Displays excellent rentention of mechanical performance at elevated temperatures. Masts and appendages. 10 hrs. at 175ºF/80ºC + optional 1 hr. at 275ºF/135ºC post cure High 220ºF/105ºC without post cure/300ºF /
150ºC with post cure		 8 weeks
CYCOM 5215 Modified epoxy prepreg. Curable at 150ºF/66ºC with only vacuum bag pressure. The cured part will yield less than 1% void content. Mechanical property and service temperature range equivalent to 1st generation epoxy prepreg after post cure at 350ºF/177ºC. Prototyping, repair, tooling and structural applications where low cost processing is desired. 14 hrs. at 150ºF/66ºC + 2 hrs. at 350ºF/177ºC post cure Low 375/191 10 days
CYCOM 5920 Modified epoxy prepreg. Formulated to cure ultra thick laminates without developing "hot spots" or runaway exotherms. Marine and submarine applications, aircraft interiors and floorings, radomes and other electronic windows. 2 hrs. at 250ºF/121ºC Medium 210/99 2 weeks
CYCOM E719 Modified epoxy prepreg. Developed specifically for marine applications and building other thick structures. Vacuum bag processable with low void content. Ship decks and components. Wind mill blades, etc. 2 hrs. at 260ºF/127ºC Medium 250/121 4 weeks
FM 753F Modified epoxy adhesive. A unique low temperature curing film adhesive. Co-curable with CYCOM 753 prepreg or with pre-cured laminates. Tough, controlled flow and gives outstanding bond strength to honeycomb cores and PVC cores. -- 8 hrs. at 140ºF/60ºC N/A 190/88 1 week
FM 754-1 Modified epoxy adhesive. Co-curable with CYCOM 754. Variable cure up to 250ºF/125ºC. -- 10 hrs. at 160ºF/70ºC Medium 195/91 3 weeks

Notes:
All of our prepreg products can be processed through the use of autoclaves, press and vacuum bag/oven.
(1) Service (operational) temperature is typically 50ºF below the glass transition temperature (Tg). Service temperature is also dependent on the stresses the structure is exposed to.

 

250ºF/121ºC Cure Adhesives

Adhesive

 Recommended Primer Description, Features and Benefits Weight Tested psf (gsm) Service Temp.
ºF/ºC		 Metal-Metal Properties Lap-Shear psi/(MPa) Metal-Metal Properties Tg ºF/ºC Composite Bonding
RT Service Temp. Floating Roller Peel pli (kN/m) RT Sandwich Peel ipp3I (Nm/m) RT Pre-Cure Co-Cure
FM 300 BR 6747-1,
BR 127 		Modified epoxy. Industry standard toughened 300ºF/149ºC service adhesive proven in metal-metal, composite and sandwich structure. Excellent surfacing characteristics. .08 (391) 300/149 5080
(35.0) 		2900
(20.0) 		29
(4.8) 		39
(58) 		296/147 Yes Yes
FM 350 NA BR 6747-1,
BR 154 		Modified epoxy. Non-asbestos structural adhesive designed for engine nacelle applications demanding continuous performance at 350ºF/177ºC. Good for reticulation applications. .10 (488) 350/177 4200
(29.0) 		3100
(21.4) 		3
(0.5) 		20
(30) 		345/174 Yes Yes
FM 355 BR 154 Modified epoxy. Adhesive film designed for composite co-cures requiring post cures. Above 400ºF/204ºC service temperature. .075 (366) 350/177 3200
(22.1) 		3000
(20.7) 		6
(1.0) 		21
(31) 		355/179 Yes Yes
FM 365 BR 6747-1,
BR 6750 		Next generation nacelle bonding adhesive. 0.06 (293) 350 (177) 4200
(29.0) 		3300
(22.8) 		12
(2.0) 		25
(37) 		374 (190) Yes Yes
FM 377 BR 6747-1,
BR 6747 		Modified epoxy. Provides excellent balance of toughness and heat age performance for both metallic and non-metallic bonded structures. Flow-controlled to provide superior reticulation characteristics, coupled with the proper balance of tack for ease of layup. .08 (391) 350/177 3925
(27.1)

2000
(13.8)

28
(4.7) 		50
(74) 		333/167 Yes Yes
FM 400 NA BR 400 Modified epoxy. 420ºF/216ºC service temperature structural adhesive for both metallic and non-metallic bonded structures. .10 (488) 420/216 4100
(28.3) 		1850
(12.8) 		8
(1.3) 		42
(62) 		352/178 Yes No
HT 424 BR 424 Modified phenolic. Extremely high service temperature adhesive capable of withstanding short term exposure to 1000ºF/538ºC. .135 (659) 500/260 3550
(24.5) 		2000
(13.8) 		10
(1.7) 		33
(49) 		358/181 Yes No
FM 1000 BR 1009-49 Polyamide. Ultra high peel strength, high elongation adhesive used extensively in metal bond helicopter blade construction. .06 (293) 180/82 6800
(46.9) 		3600
(24.8) 		140
(23.3) 		165
(245) 		257/125 Yes No
FM 1515-3 BR 6747-1,
BR 127 		Modified epoxy. Industry standard for composite bonding and surfacing applications. Designed for co-cured, pre-cured and co-bonding of composite material. Provices excellent surfacing characteristics. .05 (244) 300/149 4700
(32.4) 		1800
(12.4) 		16
(2.7) 		25
(37) 		300/149 Yes Yes
FM 1515-4 BR 6747-1,
BR 127 		Similar to 1515-3 but with 30-day out time at RT. 0.05 (244) 320 (160) 4700
(32.4) 		1500
(10.3) 		16
(2.7) 		25
(37) 		338 (170) Yes Yes


Units translation: psf=pounds per square foot; gsm=grams per square meter; pli=pounds per linear inch; kN/m=Kilonewtons per meter; ipp3I-inch pounds per 3 linear inch; Nm/m=Newton meter per meter

350ºF/177ºC Cure Adhesives

Adhesive

 Recommended Primer Description, Features and Benefits Weight Tested psf (gsm) Service Temp.
ºF/ºC		 Metal-Metal Properties Lap-Shear psi/(MPa) Metal-Metal Properties Tg ºF/ºC Composite Bonding
RT Service Temp. Floating Roller Peel pli (kN/m) RT Sandwich Peel ipp3I (Nm/m) RT Pre-Cure Co-Cure
FM 300 BR 6747-1,
BR 127 		Modified epoxy. Industry standard toughened 300ºF/149ºC service adhesive proven in metal-metal, composite and sandwich structure. Excellent surfacing characteristics. .08 (391) 300/149 5080
(35.0) 		2900
(20.0) 		29
(4.8) 		39
(58) 		296/147 Yes Yes
FM 350 NA BR 6747-1,
BR 154 		Modified epoxy. Non-asbestos structural adhesive designed for engine nacelle applications demanding continuous performance at 350ºF/177ºC. Good for reticulation applications. .10 (488) 350/177 4200
(29.0) 		3100
(21.4) 		3
(0.5) 		20
(30) 		345/174 Yes Yes
FM 355 BR 154 Modified epoxy. Adhesive film designed for composite co-cures requiring post cures. Above 400ºF/204ºC service temperature. .075 (366) 350/177 3200
(22.1) 		3000
(20.7) 		6
(1.0) 		21
(31) 		355/179 Yes Yes
FM 365 BR 6747-1,
BR 6750 		Next generation nacelle bonding adhesive. 0.06 (293) 350 (177) 4200
(29.0) 		3300
(22.8) 		12
(2.0) 		25
(37) 		374 (190) Yes Yes
FM 377 BR 6747-1,
BR 6747 		Modified epoxy. Provides excellent balance of toughness and heat age performance for both metallic and non-metallic bonded structures. Flow-controlled to provide superior reticulation characteristics, coupled with the proper balance of tack for ease of layup. .08 (391) 350/177 3925
(27.1)

2000
(13.8)

28
(4.7) 		50
(74) 		333/167 Yes Yes
FM 400 NA BR 400 Modified epoxy. 420ºF/216ºC service temperature structural adhesive for both metallic and non-metallic bonded structures. .10 (488) 420/216 4100
(28.3) 		1850
(12.8) 		8
(1.3) 		42
(62) 		352/178 Yes No
HT 424 BR 424 Modified phenolic. Extremely high service temperature adhesive capable of withstanding short term exposure to 1000ºF/538ºC. .135 (659) 500/260 3550
(24.5) 		2000
(13.8) 		10
(1.7) 		33
(49) 		358/181 Yes No
FM 1000 BR 1009-49 Polyamide. Ultra high peel strength, high elongation adhesive used extensively in metal bond helicopter blade construction. .06 (293) 180/82 6800
(46.9) 		3600
(24.8) 		140
(23.3) 		165
(245) 		257/125 Yes No
FM 1515-3 BR 6747-1,
BR 127 		Modified epoxy. Industry standard for composite bonding and surfacing applications. Designed for co-cured, pre-cured and co-bonding of composite material. Provices excellent surfacing characteristics. .05 (244) 300/149 4700
(32.4) 		1800
(12.4) 		16
(2.7) 		25
(37) 		300/149 Yes Yes
FM 1515-4 BR 6747-1,
BR 127 		Similar to 1515-3 but with 30-day out time at RT. 0.05 (244) 320 (160) 4700
(32.4) 		1500
(10.3) 		16
(2.7) 		25
(37) 		338 (170) Yes Yes

Units translation: psf=pounds per square foot; gsm=grams per square meter; pli=pounds per linear inch; kN/m=Kilonewtons per meter; ipp3I-inch pounds per 3 linear inch; Nm/m=Newton meter per meter

 

250-350ºF/121-177ºC Dual-Cure Adhesives

Film Adhesive Recommended Primer Description, Features and Benefits Weight Tested psf (gsm) Service Temp.
ºF/ºC		 Metal-Metal Properties Lap-shear psi/(MPa) Metal-Metal Properties Tg ºF/ºC Composite Bonding
RT Service
Temp.		 Floating Roller Peel pli (kN/m) RT Sandwich Peel ipp3I (Nm/m) RT Pre-Cure Co-Cure
FM 300-2 BR 6747-1,
BR 127 		Modified epoxy. 250ºF/121ºC cure version of FM® 300. Recommended for co-cured and secondary bonding of composite structures and for metal-metal bonding applications. Excellent surfacing characteristics. .08
(391) 		300
(149) 		5000
(34.5) 		2300
(15.9) 		35 (6.1) 45 (67) 290/143 Yes Yes
FM 1146 BR 6747-1,
BR 127 		Modified epoxy. Provides excellent balance of peel strength and elevated temperature performance. Designed for metal-metal bonding, pre-cured, and co-cured composite applications. .06
(293) 		250
(121) 		5800
(40.0) 		3700
(25.5) 		49 (8.6) 54 (80) 280/138 Yes Yes

Units translation: psf = pounds per square foot; gsm=grams per square meter; pli=pounds per linear inch; kN/m=Kilonewtons per meter; ipp3I-inch pounds per 3 linear inch; Nm/m=Newton meter per meter

 

Ablatives

Resin Form (1) Processing Method Description Application Features and Benefits Tensile Strength psi Tensile Strain % Cross Ply Thermal Conductivity BTU/ft-hrºF With Ply Thermal Expansion in/in/ºF
Standard and low density silica-reinforced materials
MXSE 55 BG & BT autoclave Silica fabric with elastomer modified phenolic resin. Nozzles and exit cones, external case insulation. Used where higher strain requirements are required compared to unmodified materials. 15,000 1.00 0.36 70x10-6
MXS 335B MC Compression mold Silica fabric with elastomer modified phenolic resin. Blast tube, blast deflector shield. Use where low smoke is a requirement. Also has excellent erosion properties silica-based material. 7,700 0.27 0.30 49x10-6
MXS 385 LD BG & BT Low pressure autoautoclave Low density prepreg with silica fabric and filled phenolic resin. External case insulation. Cured specific gravity as low as 1.0. 5,600 0.50 0.19 7.2x10-6
MX 2600 BG & BT Autoautoclave Silica/phenolic Nozzles for liquid rockets, blast tubes, insulators, exit cones. Widely used material with large database. Works well in oxidative environments. 12,000 0.30 0.34 76x10-6
MX 2625 MC Compression mold Silica/phenolic Small nozzles. Widely used material that molds into a variety of shapes and thicknesses. 8,500 0.30 0.32 53x10-6
FM 5504 BG & BT Autoautoclave Silica/phenolic Nozzles for liquid rockets, blast tubes, insulators, exit cones. Widely used material with large database. Works well in oxidative environments. 14,000 0.60 0.34 7.8x10-6
Standard density fiberglass-based materials
MXBE 350 BG Autoautoclave or compression Fiberglass mat with filled and elastomer modified phenolic resin. Launch canister liner. Inexpensive product with good erosion properties. 5,000 1.20 0.36 16x10-6
MXB 360 BG & BT Autoautoclave or compression Fiberglass mat with filled phenolic resin. Launch canister liner. Inexpensive product with good erosion properties. 10,000 0.25 0.40 45x10-6
MXB 6001/1584 BG & BT Autoautoclave mold Fiberglass fabric with phenolic resin. Nozzle or exit cone overwraps. High mechanical properties. 51,300 0.80 0.26 12.3x10-6
Standard and low density rayon-based carbon and graphite materials
MXG 175 BG & BT Autoautoclave Graphite (rayon) fabric with filled phenolic resin. Nozzle throat. Used when higher temperature and erosion performance required over MX 4926. 19,900 1.50 0.65 10.3x10-6
MX 4926 BG & BT Autoautoclave Carbon (rayon) fabric with filled Mil-R-9299 resin. Nozzle and exit cones. Widely used material with large database. Extensively used in large and small nozzles. 27,000 1.30 0.46 11x10-6
MX 4926 MC Compression mold Chopped carbon (rayon) fabric with filled Mil-R-9299 resin. Small nozzles. Best erosion performance of the available molding compounds. 7,500 0.25 0.53 50x10-6
MX 4957A LDC BG & BT Autoautoclave Low density rayon-based carbon. Fabric with filled phenolic. Aft exit cone. Uniform low density, mechanical/ablative properties. Specific gravity; 1.0. 15,700 1.70 0.48 30x10-6
MX 4996A BG & BT Autoautoclave Carbon fabric (rayon post woven) with filled phenolic resin. Large nozzles. Carbon fabric fired at higher temperature, greater uniformity of properties than MX 4926. 26,400 1.60 0.52 13.5x10-6
Standard and low density PAN-based carbon materials
MX 134 LDC BG & BT Autoautoclave Low density prepreg with (PAN) carbon fabric/modified phenolic. Aft exit cone. Use where light weight is desirable on aft exit cones. Specific gravity; 1.3. 44,000 1.00 0.31 43x10-6
MX 134 LDR BG & BT Autoautoclave Low density prepreg with (PAN) carbon fabric/modified phenolic. Aft exit cone. Use where light weight is desirable on aft exit cones. Specific gravity; 1.4. 39,000 0.90 0.24 --
MX 4920 BG & BT Autoautoclave T-300 (12k) fiber with filled Mil-R-9299 resin. Large nozzles and exit cones. Substitute for carbon (rayon)/phenolic where higher CTE and thermal expansion can be tolerated. 55,000 0.74 0.30 16x10-6
MX 4955 MC Compression mold T-300 (12k) fiber with filled Mil-R-9299 resin. Small nozzle. Substitute for carbon (rayon)/based phenolic where higher thermal conductivity can be tolerated. 17,000 0.25 0.51 21x10-6
FM 5879L BG & BT Autoautoclave Carbon fabric (PAN 6k) with filled phenolic. Aft exit cone. Substitute for carbon (rayon)/phenolic where higher CTE and thermal expansion can be tolerated. 66,000 0.73 0.30 18x10-6

 

High Temperature Ahesives

Film Adhesive Recommended Primer Description, Features and Benefits Weight Tested psf (gsm) Service Temp.
ºF/ºC		 Lap-Shear psi/(MPa) Tg ºF/ºC Composite bonding
RT Service Temp Pre-cure Co-cure
FM 57 BR 57 Condendsation polyimide. Non-MDA, suitable for honeycomb and wide area and heat blanket bonding. Can be cured at 350ºF/177ºC, followed by a free standing post cure. .10 (488) 550/288 3600 (24.8) 1650 (11.4) 568 (298) Yes ---
FM 680-1 BR 680 Condensation polyimide. Service temperature up to 700ºF/371ºC. Superior thermal oxidative stability. Radar transparent. Co-curable with AVIMID N polyimide and other condensation polyimide composites. .10 (488) 700/371 3000 (20.7) 1200 (8.3) 640 (338) Yes Yes
FM 2550 --- Modified BMI. Industry standard BMI developed along with CYCOM 5250-4. Suitable for both co-cure and pre-cured laminates and non-metallic core bonding. .10 (488) 400/204 3000 (20.7) 1700 (11.7) 480 (249) Yes Yes
FM 2555 --- Modified cynate ester. Low dielectric constant and loss tangent for radome applications. Developed with CYCOM® 5575-1 for use in co-cure and pre-cured laminates and non-metallic core bonding. Co-cures with most 350ºF/177ºC prepregs. .06 (293) 450/232 2700 (18.6) 3000 (20.7) 450 (232) Yes Yes

Units translation: psf=pounds per square foot; gsm=grams per square meter.

 

Foam Adhesives

Syntactic Core Description, Features and Benefits Foam Density lbs/ft3 (g/cc) Service Temp.
ºF/ºC		 Minimum Recommended Processing Conditions
FM 10

Modified epoxy. Compatible with most 350ºF/177ºC curing epoxy prepregs. Lightweight means of stiffening structures.

 40 - 42 (0.64 - 0.68) 350/177 1 hr. at 350ºF/177ºC
FM 475 Modified BMI. Syntactic foam designed to replace thin honeycomb core in the manufacture of stiff light weight panels.

40 - 45 (0.64 - 0.72)

 450/232 4 hrs. at 350ºF/177ºC and post cure
FM 6555-1 Cynate ester. Low dielectric and loss tangent foam for radome applications.

 30 - 35 (0.48 - 0.56) 350/177 6 hrs at 350ºF/177ºC and post cure

 

Aerospace Adhesives

BMI, Polyimide and Cyanate Ester Adhesives
Film adhesive Recommended primer Description, features and benefits Weight tested psf (gsm) Service temp ºF/ºC Lap-shear psi/(MPa) Tg ºF/ºC Composite bonding
RT Service temp Pre-cure Co-cure
FM® 57 BR® 57 Condendsation polyimide. Non-MDA, suitable for honeycomb and wide area and heat blanket bonding. Can be cured at 350ºF/177ºC, followed by a free standing post cure. .10 (488) 550/288 3600 (24.8) 1650 (11.4) 568 (298) Yes --
FM® 680-1 BR® 680 Condensation polyimide. Service temperature up to 700ºF/371ºC. Superior thermal oxidative stability. Radar transparent. Co-curable with AVIMID® N polyimide and other condensation polyimide composites. .10 (488) 700/371 3000 (20.7) 1200 (8.3) 640 (338) Yes Yes
FM® 2550 -- Modified BMI. Industry standard BMI developed along with CYCOM® 5250-4. Suitable for both co-cure and pre-cured laminates and non-metallic core bonding. .10 (488) 400/204 3000 (20.7) 1700 (11.7) 480 (249) Yes Yes
FM® 2555 -- Modified cyanate ester. Low dielectric constant and loss tangent for radome applications. Developed with CYCOM® 5575-1 for use in co-cure and pre-cured laminates and non-metallic core bonding. Co-cures with most 350ºF/177ºC prepregs. .06 (293) 450/232 2700 (18.6) 3000 (20.7) 450 (232) Yes Yes

Units translation: psf=pounds per square foot; gsm=grams per square meter.

 

Core Splice Adhesives

Core Splice Adhesive Description, Features and Benefits Expansion Ratio Foam Density lbs/ft3 (g/cc) Service Temp ºF/ºC Minimum Recommended Processing Conditions
FM 404 NA

Modified epoxy. Core splicing foam for use with FM 400 NA adhesive.

 4.0 - 5.0

12 - 25 (0.19 - 0.40)

 420/216 1 hr. at 350ºF/177ºC
FM 490 A

Modified epoxy. General purpose, foaming adhesive curable at 250ºF/121ºC or 350ºF/177ºC. Prevents water migration through core splicing and close outs.

 1.5 - 3.5 20 - 40 (0.32 - 0.64) 350/177 1 hr. at 250ºF/121ºC or 1 hr. at 350ºF/177ºC
FM 6604-1 Modified BMI. Low density core splice. Service temperature 350ºF/177ºC. Radar transparent and co-cures with most BMI prepregs.

 1.7 - 2.3

20 - 40 (0.32 - 0.64)

 350/177 6 hrs. at 350ºF/177ºC and post cure

 

Epoxies, Pastes and Fillers

Repair Compounds Description Features Applications Product Form Specific Gravity Work Life at R.T. Compressive Strength (psi) Minimum Recommended Processing Conditions Service Temp.
ºF/ºC		 Hardness
(Shore D)
DAPCO 3003 Thixotropic adhesive and repair compound. Flow characteristics permit use on vertical or overhead areas. General purpose; potting, honeycomb repair, composite edge filling, etc. 2 part 1.43 45 - 60 min. N/A 1 day at R.T. 225/107 85 - 90
DAPCO 3004 Rapid cure, thixotropic adhesive and repair compound. Same as above plus rapidly sandable and paintable. Same as above. 2 part 1.50 10 - 15 min. N/A 2.5 hrs. at R.T. 225/107 85 - 90
DAPCO 3005 Aerodynamic smoothing epoxy compound. Semi-thixotropic filler for metal and composite surfaces. Sandable and paintable. Available in dual pack dispenser. Same as above plus gap filling and smoothing irregular areas. 2 part 1.50 20 min. N/A 2.5 hrs. at R.T. 225/107 85 - 90
DAPCO 3008 Low density self extinguishing epoxy honeycomb filler. Excellent adhesion to a variety of substrates, can be nailed, threaded, countersunk, drilled, cut, etc. Potting, stiffening and edge filling on composite and honeycomb core. 2 part 0.45 - 0.51 90 min. 3000 6 hrs. at R.T. 225/107 60
DAPCO 3011 Fast cure low density epoxy honeycomb filler. Same as above, adhesion to an aluminum and non-metallic core. Fast curing, sandable and paintable. Same as above. 2 part 0.60 0.80 15 min. 3800 4 hrs. at R.T. 225/107 65 - 70
DAPCO 3012 Low density epoxy adhesive. Same as above, adhesion to aramid, stainless steel, and titanium. Heat removable. Available in dual pack dispenser. Bonding difficult substrates to itself and other structural materials. 2 part 0.60 45 - 60 min. 3800 6 hrs. at R.T. 225/107 60
DAPCO 3021C Low viscosity honeycomb filler. Brush, spatula, or trowel application. Excellent adhesion to aluminum, non-metallic core and wood. Potting/stiffening and edge filling of honeycomb core. Aircraft interior repair. 2 part 0.48 - 0.58 120 min. 3500 2 days at R.T. 225/107 70
DAPCO 3050 Low density, self extinguishing epoxy potting compound. Low shrinkage with excellent adhesion to metals and composites. Good compression strength. Honeycomb core filling, encapsulation and insert potting. Honeycomb core filling, encapsulation and insert potting. 1 part 28 - 30 (0.45 - 0.48) 60 days 2300 2 hrs. at 280ºF/138ºC 225/107 60

 

Potting Compounds

Foam Adhesive Description, Features and Benefits Cured Density lbs/ft3 (g/cc) Compression Strength at R.T. psi (MPa) Minimum Recommended Processing Conditions Service Temp.
ºF/ºC

BR 623-1

 Modified epoxy; one part. This family of pumpable low viscosity pastes features self-extinguishing, low smoke and toxicity for co-cure with phenolics and epoxies. Recommended for honeycomb inserts, splicing and edge close outs. 43 - 48 (0.69 - 0.77) 8000 (55.2) 1 hr. at 240º to 284ºF/116º to 140ºC -67 to 350/-55 to 177
BR 624 Microballoon filled epoxy; one part. A one component, low density material formulated for use in insert or edge filling of honeycomb sandwich construction. 37 - 47 (0.59 - 0.75) 6700 (46.2) 1 hr. at 225º to 350ºF/107º to 177ºC -67 to 350/-55 to 177
CORFIL 615 Microballoon filled epoxy; two part. Recommended for hoenycomb inserts, edging and filler, and low density moulding. 36 - 42 (0.58 - 0.67) 4700 (32.4) 75º to 350ºF/24º to 177ºC -67 to 350/-55 to 177

CORFIL 625-1

 One part, pumpable, low density epoxy paste, with nominal exotherm during either 250ºF or 350ºF cure. 25 - 31 (.40 - .50) 3000 (20.7) 1 hr. at 250ºF/121ºC to 350ºF/177ºC -67 to 350/-55 to 177

 

Resin Infusion Materials

Resin Type Features, Benefits and Applications Minimum Recommended Processing Conditions Operational
Time at
Injection Temp/Viscosity		 Relative Toughness Tg (1)
ºF/ºC Dry		 Out Life at
7ºF/25ºC
CYCOM PR 520 RTM Modified epoxy

PR 520 epoxy resin is a one-part, room temperature stable epoxy resin, requiring no mixing, engineered for resin transfer molding (RTM) processing. Low injection viscosity and unusually long out-time at ambient temperatures for a one-part resin. PR 520 offers enhanced touchness and strain-to-failure. Primary structure, secondary structure and control surfaces.

2 hrs. at 355ºF/
180ºC		 1 hour at 315ºF,
400cps		 High 160ºC 4 weeks
CYCOM 782 RTM Modified BMI

Preform binder resin fully compatible with CYCOM® 5250-4 RTM. Coated on to fabrics for the production of preforms prior to injection of CYCOM® 5250-4 RTM.

Preforming:
15 min. at
175 to 210ºF/
80 to 99ºC		 -- -- -- 12 months
CYCOM 790 RTM Modified epoxy

Preform binder resin fully compatible with CEM epoxy RTM resin systems. Novel proprietary technology ENHANCES TOUGHNESS of RTM composite structure (patent pending).

-- -- -- -- 12 months
CYCOM 823 RTM Modified epoxy >Low viscosity, room temperature injectable. Secondary aircraft structures, propeller blades and automotive components. 1 hr. at
260ºF/
127ºC		 .24 hrs. at 77ºF/25ºC / 250cps Medium 275/135 5 days
CYCOM 875 RTM Modified epoxy

Low viscosity, long out life and long injection time. Secondary aircraft structures, propeller blades.

1 hr. at
260ºF/
127ºC + 1 hr. at 355ºF/
180ºC post cure		 12 hrs. at 140ºF/60ºC / 200cps Medium 380/193 4 weeks
CYCOM 890 RTM Modified epoxy

Low viscosity, long out life and long injection times. Primary and secondary aircraft structures.

2 hrs. at
355ºF/
180ºC		 12 hrs. at 175ºF/80ºC / 250cps Medium 408/209 4 weeks
CYCOM 5250-4 RTM Modified BMI

Industry standard RTM. Low viscosity, long out life and long injection time. Versatile cure cycle is available depending on end use temperature. Post cure is required for highest thermal performance applications. Primary and secondary aircraft structures and engine components.

6 hrs. at
350ºF/
177ºC		 4 hrs. at 200 to 210ºF/95 to 99ºC / 300 cps Medium 565/296 2 weeks
CYCOM 5270 RTM Modified BMI 450ºF/232ºC continuous service BMI. Post cure required for high temperature applications. High temperature applications such as jet engine components. 4 hrs. at 350ºF/
177ºC		 2 hrs. at 200ºF/95ºC / 40ps Low 550/287 2 weeks
CYCOM 5555 RTM Modified epoxy Low moisture absorbing epoxy resin, formulated for the space industry. One part system. Typical applications include solar arrays, reflectors, optical benches, space structures, and other applications requiring very good moisture resistance. 4 hrs. at 160ºF/
320ºC		 -- -- -- 14 days
CYCOM 5575-1 RTM Modified cyanate ester Formulated specifically for the space industry. Dimensionally stable with low moisture absorption, low outgassing and low microcracking. Compatible with the usual range of reinforcing fibres, i.e. carbon, glass, aramid etc. Typical applications include space structures, and other aerospace and industrial applications requiring very good moisture resistance. 3 hrs. at 350ºF/
175ºC		 -- -- -- 14 days

RTM resins are required to be low in viscosity in order to permeate fiber preforms and to achieve fiber wet-out. This precludes the use of traditional resin toughening agents which dramatically increase viscosity and make the resin uninjectable. Cytec Engineered Materials' novel binder technology incorporates toughening agents within the binder resin which toughens the final cured component without affecting the initial RTM processing.

The toughness performance indicated are for resin + binder systems.
Epoxy binders: Preform binder systems which are fully compatible with Cytec's epoxy RTM resin systems are also available.
(1) Service (operational) temperature is typcially 50ºF below the glass transition temperature (Tg). Service temperature is also dependent on the stresses the structure is exposed to.

 

Silicone Castables

Casting Compound Tear Strength lbs/in Linear CTE in/in/ºF Volumetric CTE in-3/in-3/ºF Bulk Modulus psi Service Temp. ºF/ºC
DAPCO 1 40 1.45 x 10-4 4.35 x 10-4 2.45 x 10-4 -65 to 400 (-54 to 205)
DAPCO 10 40 1.45 x 10-4 4.35 x 10-4 2.45 x 10-4 -65 to 400 (-54 to 205)
DAPCO 37 40 1.46 x 10-4 4.38 x 10-4 2.29 x 10-4 -65 to 400 (-54 to 205)
DAPCO 38-3 60 1.01 x 10-4 3.03 x 10-4 3.33 x 10-4 -65 to 400 (-54 to 205)
DAPCO 40 75 1.51 x 10-4 4.53 x 10-4 2.37 x 10-4 -65 to 400 (-54 to 205)
DAPCO 46 150 -- -- -- -65 to 400 (-54 to 205)
DAPCO 54 50 1.48 x 10-4 4.44 x 10-4 2.49 x 10-4 -65 to 400 (-54 to 205)
DAPCO 60 50 1.25 x 10-4 3.75 x 10-4 4.13 x 10-4 -65 to 400 (-54 to 205)
DAPCO™ 1 1.45 x 10-4 4.35 x 10-4 2.45 x 10-4 -65 to 400 (-54 to 205)
DAPCO™ 10 1.45 x 10-4 4.35 x 10-4 2.45 x 10-4 -65 to 400 (-54 to 205)
DAPCO™ 37 1.46 x 10-4 4.38 x 10-4 2.29 x 10-4 -65 to 400 (-54 to 205)
DAPCO™ 38-3 1.01 x 10-4 3.03 x 10-4 3.33 x 10-4 -65 to 400 (-54 to 205)
DAPCO™ 40 1.51 x 10-4 4.53 x 10-4 2.37 x 10-4 -65 to 400 (-54 to 205)
DAPCO™ 46 -- -- -- -65 to 400 (-54 to 205)
DAPCO™ 54 1.48 x 10-4 4.44 x 10-4 2.49 x 10-4 -65 to 400 (-54 to 205)
DAPCO™ 60 1.25 x 10-4 3.75 x 10-4 4.13 x 10-4 -65 to 400 (-54 to 205)

 

Notes:



Silicone Coatings

Coating/Adhesive Description Features Applications
DAPCO 62
DAPCO 63 		Sprayable silicone rubber Can be applied by brush or spray. High elongation, low modulus. Translucent -- allows visibility through vacuum bag. For manufacturing seamless conformal vacuum bags and elastomeric tooling.
DAPCO 2030
DAPCO 2031
DAPCO 2032 		Cryongenic/thermal insulation coating Solvent borne fluoroelastomer for brush, dip or spray application. Excellent LOX compatibility, good cryogenic properties, non-burning. Hydrazine resistant. Coating for extreme temperature and chemical environments. Also used to seal backside of tools for vacuum retention.
DAPCO 3300
DAPCO 3301
DAPCO 3302 		Contact adhesive Solvent borne silicone adhesive. Bonds a veriety of substrates. Good weatherability. Increased adhesion to selected substrates using DAPCO 1-100 primer. Bonding silicone rubber and seals to many other materials. Contact adhesive for bonding fiberglass to various substrates obtaining an average of 10 pli.
DAPCO 3303 Contact adhesive VOC compliant version of 3300 series of DAPCO coatings and adhesives. Same as above.
DAPCO 3400 Silicone protective coating Solvent borne silicone coating for brush, spray or roller application. Low coefficient of friction. Extends the life of silicone vacuum bags, caul sheets, cast molds, etc., by minimizing chemical attack. Release agent on some composite parts.
DAPCO 3640 High strength/high temperature silicone adhesive tape Superior bond strength to silicones compared to liquid RTVs. Excellent tack and elastomeric properties. DAPCO primers required to bond to substrates other than silicone. Bonds substrates such as silicone rubber, metals and plastics. Easy repair of reusable vacuum bags, silicone molds, mandrels, caul plates, etc.

Coating/Adhesive Product Form RT Work Life Minimum Recommended Processing Conditions Service Temp. ºF/ºC
DAPCO 62
DAPCO 63 		2 part 1 day, 12 hrs. 24 - 72 hr. at R.T., heat acceleratable. -65º to 400ºF/-54º to 205ºC.
DAPCO 2030
DAPCO 2031
DAPCO 2032 		2 part 8 hrs. 3 days at R.T., heat acceleratable. -180º to 600ºF/-118º to 315ºC.
DAPCO 3300
DAPCO 3301
DAPCO 3302 		2 part 3 hrs. 70 % strength in 24 hrs. Full cure in 7 days. -65º to 400ºF/-54º to 205ºC.
DAPCO 3303 2 part 3 hrs. Same as above. -65º to 400ºF/-54º to 205ºC.
DAPCO 3400 1 part -- 16 hrs. at R.T. 350ºF/177ºC.
DAPCO 3640 3' catalyzed strips N/A 1 hr. at 300ºF/149ºC. -65º to 400ºF/-54º to 205ºC.

Notes:

 

Silicone Firewall Sealants

Sealant Description Features and Benefits Applications Product Form Service Temp.
ºF/ºC		 Application Time Tack Free Time Minimum Recommended Processing Conditions
DAPCO 18-4F High temp firewall sealant. Catastrophic fire protection to 2000ºF/1093ºC. Thixotropic, solvent free paste. Cure can be accelerated with heat. DAPCO™ 1-100 primer required. Fillet sealing joints for passage of fluids, air, and flame. Sealing faying surfaces of mating parts. Ablative shielding. 2 part -65º to 400ºF/ -54º to 205ºC 4 hrs. 16 hrs. 2 days at R.T.
DAPCO 72 Rapid-cure windshield sealant. Thixotropic paste with good UV and weather resistance. Fast-cure windshield repair sealant offering low adhesion. 2 part -65º to 350ºF/ -54º to 177ºC 15 min. 30 min. 4 hrs. at R.T.
DAPCO 2100 High temp primerless firewall sealant. Catastrophic fire protection to 3500ºF/1927ºC. Primerless adhesion to most substrates. Thixotropic, solvent free paste. Rapid tack free time. Fillet sealing joins for passage of fluids, air and flame. Sealing faying surfaces of mating parts. Ablative shielding. 1 part -65º to 400ºF/ -54º to 205ºC N/A 15 min. 2 days at R.T.
DAPCO 2104 Primerless general purpose, RTV sealant. Thixotropic paste with excellent primerless adhesion to hearly all substrates. Non-corrosive cure. General purpose adhesive and sealing compound. Especially for aerodynamic filleting, faying and bonding applications. 1 part -65º to 400ºF/ -54º to 205ºC N/A 30 min. 2 days at R.T.
DAPCO 2200 Rapid-cure primerless firewall sealant. Catastrophic fire protection to 2000ºF/1093ºC. Excellent adhesion to most substartes. Thixotropic, solvent free paste. Rapid cure time. Rapid-cure firewall field repairs. 2 part -65º to 400ºF/ -54º to 205ºC 30 min. 1 hr. 4 hrs. at R.T.
DAPCO 2900 High temperature ablative sealant. Catastrophic fire protection to 2000ºF/1093ºC. Thixotripic, solvent free paste. Excellent ablative properties and resistance to aviation fluids. Fillet sealing joints for passage of fluids, air, and flame. Sealing faying surfaces of mating parts. Ablative shielding. 2 part -65º to 500ºF/ -54º to 260ºC 2 hrs. 4 hrs. 2 days at R.T.

Notes:

 

Specialty Silicone Rubber: Sheets and Extrusions

Silicone Rubber Compound Features Applications Min. Recommended Processing Conditions Service Temp. ºF/ºC
SMC 250 Red cured or uncured calendered sheet and extruded shapes. High temperature tooling applications such as press molding and pressure intensifiers. 1 hr. at 340ºF/171ºC and post cure -65 to 550 (-54 to 288)
SMC 400 Translucent or red cured or uncured calendered sheet. Conforms to complex shapes. Vacuum bags, bladders and mandrels. 1 hr. at 290ºF/143ºC and post cure -65 to 400 (-54 to 205)
SMC 301 Yellow cured or uncured calendered sheet and extruded shapes. Lower cost, general purpose. (AMS 3301) 1 hr. at 290ºF/143ºC and post cure -65 to 400 (-54 to 205)
SMC 302 Yellow cured or uncured calendered sheet and extruded shapes. Lower cost, general purpose. Thermal blankets and press molding. AMS 3302, ZZR 765 Type 2A and 2B. Grade 50. 1 hr. at 290ºF/143ºC and post cure -65 to 400 (-54 to 205)
SMC 650 Yellow cured or uncured calendered sheet and extruded shapes. High tear strength. Vacuum bags, bladders and mandrels. 1 hr. at 290ºF/143ºC and post cure -65 to 400 (-54 to 205)
SMC 655FR White cured or uncured calendered sheet. Uncured catalyzed bulk rubber. Flame retardant. Compression molding of flame retardant parts. 1 hr. at 290ºF/143ºC and post cure -80 to 400 (-62 to 205)
SMC 730 Translucent cured or uncured calendered sheet. Low durometer. Available in clear smooth finish. Vacuum bags, bladders and mandrels. 1 hr. at 290ºF/143ºC and post cure -65 to 400 (-54 to 205)
SMC 731 A modified version of SMC 730 with lower potential for silicone contamination. Same as SMC 730 1 hr. at 290ºF/143ºC and post cure -65 to 400 (-54 to 205)
SMC 915 Translucent cured or uncured calendered sheet. High tear with reduced modulus. Available in clear, smooth finish. Vacuum bags, bladders and mandrels. 1 hr. at 340ºF/171ºC and post cure -65 to 400 (-54 to 205)
SMC 950 High tear strength. Translucent cured or uncured calendered sheet. Vacuum bags, bladders and mandrels. 1 hr. at 340ºF/171ºC and post cure -65 to 400 (-54 to 205)
SMC 970 High tear strength. Translucent cured or uncured calendered sheet. Vacuum bags, bladders and mandrels. 1 hr. at 340ºF/171ºC and post cure -65 to 400 (-54 to 205)
SMC 1051 Low temperature capability. Cured or uncured calendered sheet. Cryogenic processing. 1 hr. at 340ºF/171ºC and post cure -160 to 500 (-107 to 260)
SMC 1163 Blue translucent cured calendered sheet and extruded shapes. High durability. Bladders and mandrels typically used in the production of composite parts, i.e., tube claves. 1 hr. at 300ºF/149ºC and post cure -65 to 400 (-54 to 205)

Silicone Rubber Compound Specific Gravity Hardness Shore A Tensile Strength (psi)

Elongation %

 Modulus at 100% Elongation psi

Tear Strength lbs/in

Linear CTE in/in/ºF

 Compression Set %
SMC 250 1.20 50 800 400 180 75 1.51 x 10-4 25
SMC 400 1.10 30 950 800 70 130 1.83 x 10-4 30
SMC 301 1.22 40 700 500 188 60 -- 28
SMC 302 1.24 50 1000 500 -- 70 -- 20
SMC 650 1.10 50 1200 550 210 175 1.83 x 10-4 35
SMC 655FR 1.25 50 900 500 175 150 -- --
SMC 730 1.10 35 1000 750 140 150 1.75 x 10-4 35
SMC 731 1.10 30-35 1200 750 100 140 1.75 x 10-4 31
SMC 915 1.15 50 1350 850 150 200 -- 35
SMC 950 1.15 55 1400 750 330 250 1.53 x 10-4 25
SMC 970 1.22 70 1200 500 575 280 -- --
SMC 1051 1.21 50 1000 400 200 50 1.77 x 10-4 50
SMC 1163 1.15 55 1200 800 185 250 -- TBD

Notes:

 

Adhesive Materials— Complementary Products

Adhesive Description, Features and Benefits Minimum Recommended Processing Conditions Service Temp. °F/°C
SURFACE MASTER 202 Modified epoxy surfacing film providing smooth, porosity-free surface. 1.5 hrs. at 250F/121C -67 to 250/-55 to 121
SURFACE MASTER 905 Next generation epoxy surfacing film. Suitable for composite bonding. High shear and peel strengths. 1 hr. at 250° to 350°F/121° to 177°C -67 to 300/-55 to 149
FM 300 Interleaf Modified epoxy. High strain, low flow version of FM 300 developed to reduce shear stress concentrations in composite structures. Available in a wide range of thicknesses for selective interleafing. 1 hr. at 350°F/177°C -67 to 300/-55 to 149
FM 300-2 Interleaf High strain modified epoxy. 250°F/121°C to 350°F/177°C curing version of FM® 300 interleaf. Available in a wide range of thicknesses for selective interleafing. 1 hr. at 250° to 350°F/121° to 177°C -67 to 300/-55 to 149
FM 99 Modified epoxy. Mat supported adhesive film used extensively as a surfacing ply in composite structure providing a cosmetically smooth surface ready for painting. 1 hr. at 250° to 350°F/121° to 177°C -67 to 300/-55 to 149

FM 641
VERIFILM

 Modified epoxy. Non-adhering adhesive film used for tool proofing. 1 hr. at 350°F/177°C -67 to 350/-55 to 177
FM 643
VERIFILM		 Modified epoxy. 250°F/121°C curing version of FM® 641 VERIFILM® adhesive. 1.5 hrs. at 250°F/121°C -67 to 250/-55 to 121