Highly Loaded Composite Strut Test Results

Phelps, James E. ; Jegley, Dawn C. ; Wu, K. C. ; Barnard, Ansley ; McKeney, Martin J.

PID  :  NTRS Document ID: 20110008603
RP-ID  :  NF1676L-11947

学科分类：复合材料

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

Highly loaded composite struts from a proposed truss-based Altair lunar lander descent stage concept were selected for development under NASA's Advanced Composites Technology program. Predicted compressive member forces during launch and ascent of over -100,000 lbs were much greater than the tensile loads. Therefore, compressive failure modes, including structural stability, were primary design considerations. NASA's industry partner designed and built highly loaded struts that were delivered to NASA for testing. Their design, fabricated on a washout mandrel, had a uniform-diameter composite tube with composite tapered ends. Each tapered end contained a titanium end fitting with facing conical ramps that are overlaid and overwrapped with composite materials. The highly loaded struts were loaded in both tension and compression, with ultimate failure produced in compression. Results for the two struts tested are presented and discussed, along with measured deflections, strains and observed failure mechanisms.