微推进系统的MEMS技术微推力器和纳米能材料

K. Martirosyan, S. Lyshevski
{"title":"微推进系统的MEMS技术微推力器和纳米能材料","authors":"K. Martirosyan, S. Lyshevski","doi":"10.1109/MSNMC.2012.6475111","DOIUrl":null,"url":null,"abstract":"Mini and micro air vehicles, missiles, guided munitions, projectiles and ordinances are controlled by control surfaces, thrust-vectoring and varying thrust. Microthrusters are key components of some classes of flight and naval vehicles. Solid-fuel rockets and microthrusters use solid propellants. Vehicles positioning, altitude control, orbital maneuver, aerodynamic orbit phasing and rotational manoeuvres are controlled. Enabled agility and maneuverability are achieved by advanced control schemes and propulsion systems. We examine microthrusters with solid propellants for micro- and miniature flight and naval vehicles. Fundamental, applied and experimental research and technology developments are performed by devising, designing and evaluating multi-physics MEMS technology microthrusters and propulsion systems with manoenergetic materials.","PeriodicalId":394899,"journal":{"name":"2012 2nd International Conference \"Methods and Systems of Navigation and Motion Control\" (MSNMC)","volume":"37 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2012-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":"{\"title\":\"MEMS technology microthrusters and nanoenergetic materials for micropropulsion systems\",\"authors\":\"K. Martirosyan, S. Lyshevski\",\"doi\":\"10.1109/MSNMC.2012.6475111\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Mini and micro air vehicles, missiles, guided munitions, projectiles and ordinances are controlled by control surfaces, thrust-vectoring and varying thrust. Microthrusters are key components of some classes of flight and naval vehicles. Solid-fuel rockets and microthrusters use solid propellants. Vehicles positioning, altitude control, orbital maneuver, aerodynamic orbit phasing and rotational manoeuvres are controlled. Enabled agility and maneuverability are achieved by advanced control schemes and propulsion systems. We examine microthrusters with solid propellants for micro- and miniature flight and naval vehicles. Fundamental, applied and experimental research and technology developments are performed by devising, designing and evaluating multi-physics MEMS technology microthrusters and propulsion systems with manoenergetic materials.\",\"PeriodicalId\":394899,\"journal\":{\"name\":\"2012 2nd International Conference \\\"Methods and Systems of Navigation and Motion Control\\\" (MSNMC)\",\"volume\":\"37 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2012-10-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"2\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2012 2nd International Conference \\\"Methods and Systems of Navigation and Motion Control\\\" (MSNMC)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/MSNMC.2012.6475111\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2012 2nd International Conference \"Methods and Systems of Navigation and Motion Control\" (MSNMC)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/MSNMC.2012.6475111","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 2

摘要

小型和微型飞行器、导弹、制导弹药、射弹和军械由控制面、推力矢量和可变推力控制。微型推进器是某些级别的飞行器和海军飞行器的关键部件。固体燃料火箭和微型推进器使用固体推进剂。控制飞行器定位、高度控制、轨道机动、气动轨道相位和旋转机动。通过先进的控制方案和推进系统实现了灵活性和机动性。我们研究了用于微型和微型飞行和海军飞行器的固体推进剂微型推进器。基础、应用和实验研究和技术发展是通过设计、设计和评估多物理场MEMS技术微推进器和多能材料推进系统来完成的。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
MEMS technology microthrusters and nanoenergetic materials for micropropulsion systems
Mini and micro air vehicles, missiles, guided munitions, projectiles and ordinances are controlled by control surfaces, thrust-vectoring and varying thrust. Microthrusters are key components of some classes of flight and naval vehicles. Solid-fuel rockets and microthrusters use solid propellants. Vehicles positioning, altitude control, orbital maneuver, aerodynamic orbit phasing and rotational manoeuvres are controlled. Enabled agility and maneuverability are achieved by advanced control schemes and propulsion systems. We examine microthrusters with solid propellants for micro- and miniature flight and naval vehicles. Fundamental, applied and experimental research and technology developments are performed by devising, designing and evaluating multi-physics MEMS technology microthrusters and propulsion systems with manoenergetic materials.
求助全文
通过发布文献求助,成功后即可免费获取论文全文。 去求助
来源期刊
自引率
0.00%
发文量
0
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信