{"title":"用于记录航天器表面撞击的硬件概述","authors":"K. Voronov, D. Grigoriev, A. Telegin","doi":"10.51368/2307-4469-2021-9-3-245-265","DOIUrl":null,"url":null,"abstract":"A review of devices that allow detecting micrometeoroid impacts on the spacecraft body is given, namely: piezoelectric sensors, fiber-optic sensors based on Bragg gratings, resistive sensors, sensors based on solar panels, robots, video surveil-lance cameras and thermography. The advantages and disadvantages of the devic-es presented in this article, their schemes and experimental results are presented","PeriodicalId":228648,"journal":{"name":"ADVANCES IN APPLIED PHYSICS","volume":"1 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2021-08-03","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":"{\"title\":\"Overview of hardware for registering an impact on the surface of a space-craft\",\"authors\":\"K. Voronov, D. Grigoriev, A. Telegin\",\"doi\":\"10.51368/2307-4469-2021-9-3-245-265\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"A review of devices that allow detecting micrometeoroid impacts on the spacecraft body is given, namely: piezoelectric sensors, fiber-optic sensors based on Bragg gratings, resistive sensors, sensors based on solar panels, robots, video surveil-lance cameras and thermography. The advantages and disadvantages of the devic-es presented in this article, their schemes and experimental results are presented\",\"PeriodicalId\":228648,\"journal\":{\"name\":\"ADVANCES IN APPLIED PHYSICS\",\"volume\":\"1 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2021-08-03\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"2\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"ADVANCES IN APPLIED PHYSICS\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.51368/2307-4469-2021-9-3-245-265\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"ADVANCES IN APPLIED PHYSICS","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.51368/2307-4469-2021-9-3-245-265","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Overview of hardware for registering an impact on the surface of a space-craft
A review of devices that allow detecting micrometeoroid impacts on the spacecraft body is given, namely: piezoelectric sensors, fiber-optic sensors based on Bragg gratings, resistive sensors, sensors based on solar panels, robots, video surveil-lance cameras and thermography. The advantages and disadvantages of the devic-es presented in this article, their schemes and experimental results are presented