타이틀 |
Fatigue Strength of Open Hole Specimens of a T800H/PMR-15 Carbon/Polyimide Composite |
저자 |
Yasumasa HAMAGUCHI, Toshiyuki SHIMOKAWA |
Keyword |
Static Strength; Fatigue Strength; Residual Strength; PMR-15; Carbon/Polyimide composite |
URL |
http://send.nal.go.jp/send/jpn/dlpdf.php3/naltr0001392.pdf?id=NALTR0001392 |
보고서번호 |
NAL TR-1392 |
발행년도 |
1999.11 |
출처 |
NAL (National Aerospace Laboratory of Japan) |
ABSTRACT |
The objective of this study is to investigate the fatigue properties of a T800H/PMR-15 carbon/polyimide composite, selected as a candidate material for the primary structure of the unmanned space reentry vehicle HOPE-X (H-II rocket Orbiting Plane Experimental). Both static and fatigue tests were conducted to obtain data on the mechanical properties for open-hole specimens of a quasi-isotropic laminate. These tests were conducted at room temperature. The static test investigated static compression strength and static tensile strength, and the relationship between open-hole deformation and load was also examined. The fatigue test investigated S-N relationships for stress ratios R=0.1,R=-infinity and R=-1, and the residual strength of the non-failure specimens. The fatigue damage process arising from the relationship between number of cycles and open-hole deformation was also investigated. The results of analysis and evaluation of the strength characteristic obtained from these tests is reported. |