2004 IEEE Aerospace Conference Proceedings (IEEE Cat. No.04TH8720)
DOI: 10.1109/aero.2004.1368050
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Application of commercial electronics in the motors and actuator systems for mars surface missions

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Cited by 3 publications
(2 citation statements)
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“…The monitoring and data recording for electrical continuity was a continuous scan during the temperature cycling. Details of the selection process and assembly testing and analysis, including the design of the test vehicles, test set-up and continuous monitoring, detailed test results, wire bond modeling, failure analysis with SEM cross-section images, and some materials combination suggestions can be found in the references [3][4][12][13][14][15]. This paper is focused on the qualification process for the technology development with the summary of the results.…”
Section: B Assembly Boardmentioning
confidence: 99%
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“…The monitoring and data recording for electrical continuity was a continuous scan during the temperature cycling. Details of the selection process and assembly testing and analysis, including the design of the test vehicles, test set-up and continuous monitoring, detailed test results, wire bond modeling, failure analysis with SEM cross-section images, and some materials combination suggestions can be found in the references [3][4][12][13][14][15]. This paper is focused on the qualification process for the technology development with the summary of the results.…”
Section: B Assembly Boardmentioning
confidence: 99%
“…A functional go/no-go testing on the electronics down to as low as -180°C was first conducted to characterize the electronics at low temperatures [3][4]. While the majority of the electronics selected were functional and survived the low temperature test, all the op-amps tested failed to meet the performance requirements of the assembly over the wide temperature range.…”
Section: A Electronicsmentioning
confidence: 99%