Design and Test of Retention Mechanism to Apply Direction-Dependent Axial Force to Mars Returnable Sample Tube Assemblies
收藏DataCite Commons2024-05-19 更新2025-04-16 收录
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http://dataverse.jpl.nasa.gov/citation?persistentId=doi:10.48577/jpl.PM9OWT
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资源简介：
This paper describes a compact, high force, fully reversible 2-way latching mechanism design that will interact with hardware currently on Mars. Details of the mechanism and a novel wire wound joint design are presented alongside preliminary test results and lessons learned. A hardware-rich, iterative design approach has informed the design, which has potential applications for future high-reliability aerospace latch mechanisms.
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Root
创建时间：
2024-05-19
