ReliabilityAssessmentMethodforSolarArrayDeploymentofSpacecraft

doi:10.3780/j.issn.1000-758X.2013.03.008

Abstract

Abstract: Aselectricpowersupplydevicesofspacecraft,solararrayshaveplayedanimportantroleinassuringsuccessfulspaceflight.Basedontheanalysisofsomecharacteristicparametersofsolararraydeploymentprocess,theequivalentdrivingmomentobtainedfromeveryhingedrivingmomentmeasurementvaluewasselectedasreliabilitycharacteristicparameterofsolararraydeployment.Bystressstrengthinterferencetheory,areliabilityassessmentmethodwasputforwardwhichapplinghingemeasurementdataofbothdrivingmomentandresistancemomenttoreliabilityassessmentofthesolararraydeployment.Thismethodprovidesatechnicalapproachtovalidatethereliabilityofspacecraftsolararraydeployment.

Key words: Reliabilityassessment, Solararray, Deployment, Spacecraft

LIU Zhi-Quan, WU Yue-Min, PU Hai-Ling, YANG Qiao-Long. ReliabilityAssessmentMethodforSolarArrayDeploymentofSpacecraft[J]. , 2013, 33(3): 52-56.

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URL: http://journal26.magtechjournal.com/kjkxjs/EN/10.3780/j.issn.1000-758X.2013.03.008

http://journal26.magtechjournal.com/kjkxjs/EN/Y2013/V33/I3/52

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ReliabilityAssessmentMethodforSolarArrayDeploymentofSpacecraft

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