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 BMI Prepreg System with AS4-3K-70PW Woven Carbon Fiber
Categories: Polymer; Thermoset; Bismaleimide (BMI); Carbon Fiber/Thermoset Composite

Material Notes: 58 Volume % AS4-3K-70PW.

CYCOM® 5250-4 is a 350°F to 400°F (177°C to 204°C) curing bismaleimide resin with a service temperature range of -75°F to 400°F (-59°C to 204°C). CYCOM 5250-4 is specifically formulated for use in primary aircraft structures. In addition, a variety of secondary structural components can take advantage of the increased performance from using high-strain carbon fibers and the improved damage-resistance this system provides. CYCOM 5250-4 is available with either carbon fiber or glass fiber reinforcement in unidirectional tape, woven broadgood and roving forms.

Features & Benefits:

  • Short-term service temperature up to 450°F (232°C)
  • Superior hot/wet properties at 220°F to 375°F (104°C to 190°C)
  • Excellent toughness
  • Void-free laminates
  • High temperature resistance
  • Low thermal conductivity
  • Versatile cure
  • Excellent compression strength properties after impact
  • Shop life greater than 28 days at room temperature
  • Fluid/solvent resistant
Suggested Applications: Primary and secondary aircraft structure including:
  • Engine nacelles
  • Fuselage skins and stiffeners
  • Wing and stabilizer spars and skins
  • Other critical load-bearing components
Mechanical properties are reported for standard cure + standard post-cure

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
Density 1.25 g/cc0.0452 lb/in³Neat Resin; QC-PT-55
Volatiles 2.0 %2.0 %
Water Absorption 1.3 %
@Temperature 149 °C
1.3 %
@Temperature 300 °F
As Tested (Wet)
 
Mechanical PropertiesMetricEnglishComments
Tensile Strength 848 MPa
@Temperature 24.0 °C
123000 psi
@Temperature 75.2 °F
Warp (0°), AS4-3K-70PW; ASTM D3039
Tensile Modulus 70.0 GPa
@Temperature 24.0 °C
10200 ksi
@Temperature 75.2 °F
Warp (0°), AS4-3K-70PW
Compressive Strength  242 MPa
@Temperature 149 °C
35100 psi
@Temperature 300 °F
Open Hole, [(+/-45),(0/90)], AS4-3K-70PW, WET
 269 MPa
@Temperature 177 °C
39000 psi
@Temperature 351 °F
Open Hole, [(+/-45),(0/90)], AS4-3K-70PW
 297 MPa
@Temperature 121 °C
43100 psi
@Temperature 250 °F
Open Hole, [(+/-45),(0/90)], AS4-3K-70PW
 310 MPa
@Temperature 24.0 °C
45000 psi
@Temperature 75.2 °F
Open Hole, [(+/-45),(0/90)], AS4-3K-70PW
 448 MPa
@Temperature 177 °C
65000 psi
@Temperature 351 °F
Warp (0°), AS4-3K-70PW, Wet; SACMA SRM 1-88
 759 MPa
@Temperature 163 °C
110000 psi
@Temperature 325 °F
Warp (0°), AS4-3K-70PW; SACMA SRM 1-88
 862 MPa
@Temperature 24.0 °C
125000 psi
@Temperature 75.2 °F
Warp (0°), AS4-3K-70PW; SACMA SRM 1-88
Compressive Modulus 61.0 GPa8850 ksiWarp (0°), AS4-3K-70PW
Shear Strength  41.4 MPa
@Temperature 177 °C
6000 psi
@Temperature 351 °F
Short Beam Warp, AS4-3K-70PW, Wet
 49.0 MPa
@Temperature 177 °C
7100 psi
@Temperature 351 °F
Short Beam Warp, AS4-3K-70PW
 63.4 MPa
@Temperature 121 °C
9200 psi
@Temperature 250 °F
Short Beam Warp, AS4-3K-70PW
 69.6 MPa
@Temperature 24.0 °C
10100 psi
@Temperature 75.2 °F
Compression Interlaminar Warp (0°), AS4-3K-70PW
 71.7 MPa
@Temperature 24.0 °C
10400 psi
@Temperature 75.2 °F
Short Beam Warp, AS4-3K-70PW
 
Thermal PropertiesMetricEnglishComments
Maximum Service Temperature, Air 204 °C400 °FContinuous; depends on cure cycle
 232 °C450 °Fshort term; depends on cure cycle
Minimum Service Temperature, Air -59.4 °C-75.0 °F
Glass Transition Temp, Tg 200 °C392 °FWet; QC-PT-22
 216 °C421 °FPost Cure: 177°C for 6 hrs
 249 °C480 °FPost Cure: 190°C for 6 hrs
 263 °C505 °FPost Cure: 210°C for 6 hrs
 282 °C540 °FPost Cure: 227°C for 6 hrs
 300 °C572 °FDry; QC-PT-22
 304 °C579 °FPost Cure: 243°C for 6 hrs
 
Processing PropertiesMetricEnglishComments
Processing Temperature 177 - 204 °C350 - 400 °FCure Temperature - Autoclave
Gel Time 65.0 min
@Temperature 177 °C
65.0 min
@Temperature 351 °F
in nitrogen atmosphere; QC-TP-87
Shelf Life  >= 1.00 Month
@Temperature 72.0 °C
>= 1.00 Month
@Temperature 162 °F
 >= 3.00 Month
@Temperature 4.44 °C
>= 3.00 Month
@Temperature 40.0 °F
 >= 12.0 Month
@Temperature -17.8 °C
>= 12.0 Month
@Temperature 0.000 °F

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 BMI Prepreg System with G30-500-3K-8HS Woven Carbon Fiber
Solvay CYCOM® 5250-4 BMI Prepreg System with G30-500-3K-70PW Woven Carbon Fiber
Solvay CYCOM® 5250-4 BMI Prepreg System with IM-7 Carbon Fiber
Solvay CYCOM® 5250-4 BMI Prepreg System with G40-800 Carbon Fiber
Solvay CYCOM® 5250-4 BMI Prepreg System with G30-500 Carbon Fiber

PCYTED133_4 / 192680

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.