LR 1504 - 19 osy 8HS Silica Ablative Prepreg - Lewcott - #1

/ 1


catalogue search
LR 1504 - 19 osy 8HS Silica Ablative Prepreg - Lewcott
P. 01
Page:
LR 1504 - 19 osy 8HS Silica Ablative Prepreg - Lewcott


See other catalogues for Lewcott

Text version of the page
86 Providence Rd • Millbury, MA 01527 (800) 225-7725 • www.lewcott.com
LR1504 Prepreg
LR1504 is a composite produced from a silica filled Lewcott PSR133 MIL-R-9299 phenolic resin matrix on a 18 osy high silica fabric. The material is designed to meet and/or exceed the thermal and insula­tion requirements of solid and liquid propulsion rockets.
Chemical Properties of LR1504 Prepreg
Property
Value
Test Method
Resin Solids, %
29-33
QCP-R-7
Volatile, %
3-7
QCP-V-1
Laminar Flow @ 150 psi, %
6-15
QCP-F-1
Filler Content, %
6-10
QCP-R-5
Uncured Thickness, x10-3 in.
0.039
QCP-T-2
Prepreg Width, in
33
Physical Properties of LR1504
Property Value
Specific Gravity 1.71
Tensile Strength, psi 12,000
Tensile Modulus, msi 2.0
Tensile Elongation, % 0.5
Flexural Strength, psi 21,000
Flexural Modulus, msi 2.6
Compression Strength, psi 35,000
Interlaminar Shear Strength, psi 8,000
Test Method
ASTM-D-792
ASTM-D-638 ASTM-D-638 ASTM-D-638 ASTM-D-790
ASTM-D-790 ASTM-D-695
FTMS401/1041
Thermal Conductivity (across ply), BTU/ 0.23 ft.-hr.-oF
ASTM-C-177
ASTM-C-351
Specific Heat @ 150oF, BTU/lb. oF
0.22
0.024
Cured Ply Thickness, in.
Molding Cycle
Press cured at 325oF using 1000 psi pressure for 2 hours.
NOTE: The data presented herein has been developed under controlled manufacturing and test conditions and is considered accurate. No warranty is expressed or implied regarding the accuracy or use of this data or the use of this product. It is the responsibility of the end user to determine suitability for use. Rev. Date: 6/07

pageCatalog pdf di En 2012-02-07-15