... (m/m/°C, in./in./°F)
MIL- HDBK- 17- 4
Volume 4 of 4
21 September 1999
DEPARTMENT OF DEFENSE
HANDBOOK
COMPOSITE MATERIALS HANDBOOK
VOLUME 4. METAL MATRIX COMPOSITES
This handbook is for guidance ... fusion processes.
MIL- HDBK- 17- 4
7
Further discussions of these and other issues are provided in Section 2. Specific uses of handbook data
are beyond the scope and...
... MIL-HDBK-17-4
57
1.2 .3. 3.4
Magnesium
This section is reserved for future use.
1.2 .3. 3.5
Nickel
This section is reserved for future use.
1.2 .3. 3.6
Titanium
Titanium matrix composites have been ... condition of 73 5°F ( 23 3 C) at ambient
laboratory relative humidity; 2) a material condition where, immediately following consolidation/cure, the
material is stored at 73 5°F ( 23 3 C)...
... Joining Techniques for Metal
Matrix Composites,” Boeing Co., Report: AMMRC TR- 84- 35, August 19 84.
1.2.8 .4. 3 .4( a) Nedervelt, P. D., and Burns R. A., “Metal Matrix Composites Joining and Assembly
Technology,” ... Report No. WL-TR-93 -40 83, September 1993.
1.2.8 .4. 3 .4( b) Lienert, T., Lane, C., and Gould, J., “Selection and Weldability of Al. Metal Matrix
Composites,” ASM Handbook,...
... Metal Matrix
Composites,” Annual Book of ASTM Standards, Vol 15.03, American Society for Testing
and Materials, West Conshohocken, PA, 19 97, pp. 173 - 177 .
1.4.2.2 ASTM Standard D3410- 87, "Standard ... to be located along a constant ge-
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94
MIL-HDBK -73 1 Thermography
MIL-HDBK -73 2 Acoustic Emission
MIL-HDBK -73 3 Radiography
MIL-HDBK -78 7 Ultrasonic
These documents...
... matrix manufacture Date of data submittal 6 /98
Date of testing 5 /96 -7 /97 Date of analysis 8 /98
MATRIX PROPERTY SUMMARY
Temperature 75°F 400°F 600°F 800°F 90 0°F 1000°F
Environment Air
(1)
Air Air ... (2)
F
tu
Distribution ANOVA
(ksi) C
1
2. 89
C
2
12 .9
No. Specimens 7
No. Lots 2
Approval Class Screening
Mean 12.4 12.3 11.4
Minimum 11 .9 12.0
Maximum 13.0 12.6
E
t
C.V.(%) 3. 39
(M...
... applica-
bility of this method for various composite systems. However, Tables A1(a) and A1(b) in Appendix A pro-
vide some useful information on the SCS -6/ Ti-24-11 composite system, in addition to giving ... is to
test thicker materials which can withstand compressive loads. This may not be an option due to the high
cost of thick materials or difficulties in manufacturing thick comp...
... of interfacial failure pos-
sible.
MIL-HDBK-1 7-4
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FIGURE 1.4.2.13.5(b)
Tabletop fiber pushout testing system used at NASA Lewis Research Center.
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ments. A sudden divergence ... complete removal of the fiber.
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FIGURE 1.4.2.5(a)
Middle tension specimen, M (T).
FIGURE 1.4.2.5(b)
Single-edge tension specimen, SE (T).
MIL-HDBK-1 7-4...