Failure analysis of a vibration isolator used in launch vehicle applications

S.V.S. Narayana Murty, Sushant K. Manwatkar, P. Ramesh Narayanan
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引用次数: 1

Abstract

Vibration isolators are used in launch vehicles to protect sensitive electronic equipments from the rigors of flight structural vibrations during the lift-off and ascent phase. Failure of one such vibration isolator made of AISI 304 is reported in the present study after ground level testing has been completed. The vibration isolator had a crack of length approximately 42 mm at the fore end corner. Detailed optical and scanning electron microscopy was conducted on the failed vibration isolator to understand the reasons for cracking. Finally, it was concluded that micro cracks formed during the deep drawing operation (due to large strains at the fore end corner) propagated during vibration testing resulting in the failure of the body of the vibration isolator.

运载火箭用隔振器失效分析
在运载火箭的发射和上升阶段,隔振器用于保护敏感的电子设备免受飞行结构振动的影响。在地面测试完成后,本研究报告了一个由AISI 304制成的此类隔振器的失效。隔振器在前端角处有一条长度约为42 mm的裂缝。对失效隔振器进行了详细的光学和扫描电镜观察,了解其开裂原因。最后得出结论,在拉深过程中形成的微裂纹(由于前端角处的大应变)在振动测试过程中传播,导致隔振器本体失效。
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