ORION - Crew Module Side Hatch: Proof Pressure Test Anomaly Investigation

Evernden, Brent A ; Guzman, Oscar J

关键词: CREW EXPLORATION VEHICLE;    SPACECRAFT MODULES;    SPACECREWS;    HATCHES;    PRODUCT DEVELOPMENT;    PROVING;    STRUCTURAL STABILITY;    ABNORMALITIES;    LEAKAGE;    LESSONS LEARNED;   

RP-ID  :  JSC-CN-40662

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

The Orion Multi-Purpose Crew Vehicle program was performing a proof pressure test on an engineering development unit (EDU) of the Orion Crew Module Side Hatch (CMSH) assembly. The purpose of the proof test was to demonstrate structural capability, with margin, at 1.5 times the maximum design pressure, before integrating the CMSH to the Orion Crew Module structural test article for subsequent pressure testing. The pressure test was performed at lower pressures of 3 psig, 10 psig and 15.75 psig with no apparent abnormal behavior or leaking. During pressurization to proof pressure of 23.32 psig, a loud 'pop' was heard at ~21.3 psig. Upon review into the test cell, it was noted that the hatch had prematurely separated from the proof test fixture, thus immediately ending the test. The proof pressure test was expected be a simple verification but has since evolved into a significant joint failure investigation from both Lockheed Martin and NASA.