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0001a4a31c369c6418707c7e2ce6e6ef75a68adc | AMS_2018.pdf | 323 | simply reinforce good system and test design practice. The following recommendations are made based on the issues encountered during CSADA qualification. •When performing shock tests on slip rings, care should be taken to avoid an excessive shock pulse duration, excessive displacement, and over-exposure in the lower... | [
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00053953623d054747d255c6cd28c089854ab4b5 | AMS_2018.pdf | 473 | mechanisms test. Electrical pinout verification is made much easier with automated harness testers. These automated testers make harness testing as simple as plugging the harness into the tester which uses a computer driven electronic tester to very rapidly perform all the resistance, continuity, dielectric and HiPo... | [
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0009a16bdab4f2763980e652e22c9abaa96c1762 | AMS_2018.pdf | 235 | design guidelines exist. This paper aims to quantify locking and to help answer the question “What moment does a secondary locking feature need to provide to prevent loosening?” Self-Loosening Moment Threaded fasteners exhibit an inherent self-loosening moment. This self-loosening moment is evident from the torque... | [
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000cad7233c3c63ac61a0f06474f18d0f50184e6 | AMS_2020.pdf | 153 | be used on the flight unit, to an axial load near to that of the flight units max capability, and to a cross -moment ranging from matching the flight expected load to 4X that , see Figure 11 and Figure 13. Both lubricated and nonlubricated ram t ips were used, and each was tested pas t 1X life. No degradation in the ... | [
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001186298ba7a8f8570a5febd7fc9f3d7b362616 | AMS_2018.pdf | 490 | spacecraft docking harkens back to the days of wind-driven ships. Docking, berthing, ports and other mating system terminology are vestiges of our maritime traditions. The special allure of spacecraft docking is evident in popular culture. Most space travel motion pictures inevitably include a detailed technical sce... | [
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0011e034a24f29562d42b9bbf26fe68bb114af28 | AMS_2020.pdf | 45 | "Figure 7. Exterior View of the C rack One possible root cause for this crack is stress concentrati(...TRUNCATED) | [0.004379947204142809,-0.007647957187145948,-0.002125562634319067,-0.02390664629638195,-0.0039121201(...TRUNCATED) | doc | [] | 0 | null | null | null | null | null | null |
001839d3c8b21537be890d4cda7fca528fa48c8a | AMS_2018.pdf | 405 | "the issue, which it passed. The redesign was then reinstalled on the flight hardware and underwent(...TRUNCATED) | [0.0069140782579779625,0.021124418824911118,-0.026933634653687477,0.0019335097167640924,-0.012890065(...TRUNCATED) | doc | [] | 0 | null | null | null | null | null | null |
001bb8e0950fc993b461d544372d531962780fd2 | AMS_2018.pdf | 310 | "test the motors in the correct thermal and vacuum environment are difficult to find on center witho(...TRUNCATED) | [-0.02064008079469204,-0.0057280645705759525,-0.009428856894373894,-0.028245754539966583,-0.00677231(...TRUNCATED) | doc | [] | 0 | null | null | null | null | null | null |
001ec0d154612eedbdcc7cca4dde94e01fe6b31f | AMS_2018.pdf | 128 | "affected the preload, starting torque, running torque or runout. Drive electronics to be used for (...TRUNCATED) | [-0.03805001080036163,-0.007127393037080765,-0.008080738596618176,-0.017041487619280815,-0.035479821(...TRUNCATED) | doc | [] | 0 | null | null | null | null | null | null |
002c17eef38ec942554fd79e0935a507288458d8 | AMS_2018.pdf | 165 | "µavg = 0.2 measured in the 30°C experiments was insufficient to generate enough local heating of(...TRUNCATED) | [0.0032210343051701784,0.0051625263877213,0.009867829270660877,-0.020049573853611946,-0.018821213394(...TRUNCATED) | doc | [] | 0 | null | null | null | null | null | null |
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