Publication Date:
2019-07-13
Description:
Cracks were detected in flow liners at the gimbal joints in the LH2 feedlines of the space shuttle's main engines. The cracks initiated at defects in the drainage slots of the flow liners and grew due to high cycle fatigue. Fracture mechanics analyses were conducted to evaluate the life of the liners. These analyses yielded extremely short lives in the presence of small surface or corner cracks. A high fidelity detection method, edge replication, was used to detect the very small cracks. The detected cracks were removed by polishing and the surface quality of the slots was reestablished to improve life of the liners.
Keywords:
Spacecraft Design, Testing and Performance
Type:
ICCES 2005 - International Conference on Computational & Experimental Engineering and Sciences; Dec 01, 2005 - Dec 06, 2005; Chennai; India
Format:
application/pdf
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