MatWeb - Material Property Data Advertise with MatWeb!     Register Now
Data sheets for over 180,000 metals, plastics, ceramics, and composites.
MatWeb - Material Property Data HOME  •   SEARCH  •   TOOLS  •   SUPPLIERS  •   FOLDERS  •   ABOUT US  •   FAQ  •   LOG IN    
Recently Viewed Materials (most recent at top)  

Login to see your most recently viewed materials here.

Or if you don't have an account with us yet, then click here to register.

  Searches:   Advanced  | Category  | Property  | Metals  | Trade Name  | Manufacturer  | Recently Viewed Materials
  

Ensinger PEI

Solvay CYCOM® 5250-4 RTM BMI Resin, Composite with T650-35-3K-PW Fabric
Categories: Polymer; Thermoset; Bismaleimide (BMI); Carbon Fiber/Thermoset Composite

Material Notes: CYCOM® 5250-4 RTM is a true one-part homogeneous BMI resin developed specifically for the resin transfer molding (RTM) process. It reaches very low viscosity during transfer and maintains a low viscosity for several hours, thus providing the maximum capability to fabricate complex parts. Laminates fabricated from CYCOM 5250-4 RTM are capable of service temperatures up to 400°F (204°C), but its toughness and processability make it an ideal material for 180°F (82°C) temperature applications where epoxies are commonly used. CYCOM 5250-4 RTM offers the highest open hole compression (OHC) value of any organic matrix resin while providing the highest level of toughness available in an RTM capable matrix resin.

Features & Benefits:

  • Excellent toughness
  • Maximum continuous service temperature up to 400°F (204°C)
  • Superior hot/wet properties at 160 to 375°F (71 to190°C)
  • Low viscosity during processing
  • Low-tack, solid at room temperature provides ease of handling
  • Low thermal conductivity
  • Versatile cure, can be cured at 400°F (204°C) for 2 hours
  • Out-time greater than 60 days at room temperature
  • True one-part formulation
  • Fully compatible CYCOM 5240-4 RTM low resin content prepregs and CYCOM 782 RTM bindercoated fabrics are available for preform manufacture
Applications:
  • Wing stabilizer spars
  • Fuselage skins and stiffeners
  • Low operating temperature, critical load-bearing components
  • Engine components
Mechanical properties for composites with 58% fiber volume T650-35-3K-PW carbon fiber fabric, after standard cure + postcure.

Information provided by Cytec, subsequently acquired by Solvay.

Vendors: No vendors are listed for this material. Please click here if you are a supplier and would like information on how to add your listing to this material.
 
Physical PropertiesMetricEnglishComments
Water Absorption  3.9 %
@Temperature 71.1 °C,
Time 3.60e+6 sec
3.9 %
@Temperature 160 °F,
Time 1000 hour
Neat resin after 400°F cure (no postcure)
 4.2 %
@Temperature 71.1 °C,
Time 3.60e+6 sec
4.2 %
@Temperature 160 °F,
Time 1000 hour
Neat resin after standard cure + postcure
 
Mechanical PropertiesMetricEnglishComments
Flexural Strength  586 MPa
@Temperature 177 °C
85000 psi
@Temperature 351 °F
Fill 90° Direction, wet
 621 MPa
@Temperature 177 °C
90000 psi
@Temperature 351 °F
Warp 0° Direction, wet
 1020 MPa
@Temperature 25.0 °C
148000 psi
@Temperature 77.0 °F
Fill 90° Direction
 1070 MPa
@Temperature 25.0 °C
155000 psi
@Temperature 77.0 °F
Warp 0° Direction
Flexural Modulus  60.7 GPa
@Temperature 177 °C
8800 ksi
@Temperature 351 °F
Warp 0° Direction, wet
 62.1 GPa
@Temperature 177 °C
9010 ksi
@Temperature 351 °F
Fill 90° Direction, wet
 62.1 GPa
@Temperature 25.0 °C
9010 ksi
@Temperature 77.0 °F
Warp 0° Direction
 62.1 GPa
@Temperature 25.0 °C
9010 ksi
@Temperature 77.0 °F
Fill 90° Direction
Compressive Strength 220 MPa31900 psiafter 1500 in-lb/in impact
Shear Strength  40.7 MPa
@Thickness 4500 mm
5900 psi
@Thickness 177 in
Short beam, Warp 0° Direction, wet
 70.3 MPa
@Thickness 635 mm
10200 psi
@Thickness 25.0 in
Short beam, Warp 0° Direction
 
Thermal PropertiesMetricEnglishComments
Maximum Service Temperature, Air 204 °C399 °Fcontinuous
Glass Transition Temp, Tg 199 °C390 °F204°C for 2 hrs-no postcure, wet
 207 °C405 °FStandard Cure+Standard Postcure, wet
 254 °C489 °F204°C for 2 hrs-no postcure, dry
 271 °C520 °FStandard Cure+Standard Postcure, dry
 
Processing PropertiesMetricEnglishComments
Processing Temperature  177 - 191 °C
@Time 21600 sec
350 - 375 °F
@Time 6.00 hour
Standard Cure. Standard post cure is 440°F for 4 hours
 <= 204 °C
@Time 7200 sec
<= 400 °F
@Time 2.00 hour
optional cure (no postcure)
Gel Time 35.0 min
@Temperature 177 °C
35.0 min
@Temperature 351 °F
neat resin
Shelf Life 6.00 Month
@Temperature <=-17.8 °C
6.00 Month
@Temperature <=0.000 °F
sealed container, neat resin

Some of the values displayed above may have been converted from their original units and/or rounded in order to display the information in a consistent format. Users requiring more precise data for scientific or engineering calculations can click on the property value to see the original value as well as raw conversions to equivalent units. We advise that you only use the original value or one of its raw conversions in your calculations to minimize rounding error. We also ask that you refer to MatWeb's terms of use regarding this information. Click here to view all the property values for this datasheet as they were originally entered into MatWeb.

Users viewing this material also viewed the following:
Solvay CYCOM® 5250-4 RTM BMI Resin, Composite with IM7-6K-4HS Fabric
Solvay CYCOM® 381 Epoxy Prepreg with IM7 Uni-graphite and 148FAW Epoxy
Solvay CYCOM® 5320-1 Epoxy with T40/800B Unidirectional Tape Composite
Solvay CYCOM® 890 RTM Resin - Woven Carbon Fabric Composite
Solvay CYCOM® 977-3 Epoxy - Unidirectional Carbon Fiber Tape

PCYTED079a / 233831

Proto3000 – 3D Engineering Solutions

Please read our License Agreement regarding materials data and our Privacy Policy. Questions or comments about MatWeb? Please contact us at webmaster@matweb.com. We appreciate your input.

The contents of this web site, the MatWeb logo, and "MatWeb" are Copyright 1996-2024 by MatWeb, LLC. MatWeb is intended for personal, non-commercial use. The contents, results, and technical data from this site may not be reproduced either electronically, photographically or substantively without permission from MatWeb, LLC.