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浅析星型涤锦复合纤维纺丝工艺 被引量:2
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作者 洪剑桥 刘学峰 +1 位作者 刘先正 肖刚 《合成纤维工业》 CAS CSCD 北大核心 2002年第4期42-44,共3页
探索了 PET/ PA6星型复合纤维纺丝工艺 ,讨论了两组分复合比、纺丝温度、拉伸倍率、拉伸温度等条件对复合纤维的生产过程及产品质量的影响。认为选择 PET/ PA6复合比为 80 / 2 0 ,纺丝温度2 80~ 2 90℃ ,拉伸温度 80~ 90℃ ,定型温度 ... 探索了 PET/ PA6星型复合纤维纺丝工艺 ,讨论了两组分复合比、纺丝温度、拉伸倍率、拉伸温度等条件对复合纤维的生产过程及产品质量的影响。认为选择 PET/ PA6复合比为 80 / 2 0 ,纺丝温度2 80~ 2 90℃ ,拉伸温度 80~ 90℃ ,定型温度 190~ 2 0 0℃ ,纺丝顺利 ,产品质量较好。 展开更多
关键词 析星型 涤锦复合纤维 PET/PA6 纺丝工艺
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Design and analysis of the reliability of on-board computer system based on Markov-model
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作者 马秀娟 曹喜滨 赵国良 《Journal of Harbin Institute of Technology(New Series)》 EI CAS 2005年第1期17-20,共4页
An on-board computer system should have such advantages as light weight,small volume and low power to meet the demand of micro-satellites. This paper, based on specific characteristics of Stereo Mapping Micro-Satellit... An on-board computer system should have such advantages as light weight,small volume and low power to meet the demand of micro-satellites. This paper, based on specific characteristics of Stereo Mapping Micro-Satellite (SMMS), describes the on-board computer system with its advantage of having centralized and distributed control in the same system and analyzes its reliability based on a Markov model in order to provide a theoretical foundation for a reliable design. The on-board computer system has been put into use in principle prototype model of Stereo Mapping Micro-Satellite and has already been debugged. All indexes meet the requirements of the design. 展开更多
关键词 markov model computer system RELIABILITY MICRO-SATELLITE
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Risk Analysis Comparison between the Mission NANOSATC-BR1 and NANOSATC-BR2
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作者 Marcos Antonio Laurindo Dal Piaz Lucas Lourencena Caldas Franke +5 位作者 Mauricio Ricardo Balestrini Iago Camargo Silveira Guilherme Paul Jaenisch Tiago Travi Farias Otavio Santos Cupertino Durao Nelson Jorge Schuch 《Journal of Mechanics Engineering and Automation》 2015年第2期88-94,共7页
The goal of this work is to perform the risks analysis of the mission NANOSATC-BR1 and NANOSATC-BR2 and then compare them linearly. The NANOSATC-BR1 and NANOSATC-BR2 are the first and the second satellite, respectivel... The goal of this work is to perform the risks analysis of the mission NANOSATC-BR1 and NANOSATC-BR2 and then compare them linearly. The NANOSATC-BR1 and NANOSATC-BR2 are the first and the second satellite, respectively. They belonged to the project NANOSATC-BR-development of CubeSats, which is performed in the facilities built by the partnership between the National Institute of Space Research and the Technological Center from Federal University of Santa Maria. The project focuses on the development of a scientific instrumentation and, simultaneously, the design development, construction, qualification and launch of a national scientific nanosatellite, in a cube shape with 100 mm of edge and near to 1.33 kg of mass, per unit (U). The risk analysis was held to identify and minimize the project's risks of failure, due to its complexity, assuring the mission success, preventing extra pays and rework. The software, CubeSat Mission Design Software Tool for Risk Estimating, which uses statistical regression methods, was used. So, we were capable to measure the project's most critical steps assuring its success. The NANOSATC-BR1 was launched in June 19 and it is orbiting the Earth in a nominal regime and the NANOSATC-BR2 has been scheduled to be launched in 2016. 展开更多
关键词 Analysis RISK CubeSat.
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Technology and Market Prospect Analysis of Low Cost Small-lift Launch Vehicles for Small Satellites
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作者 YAO Yanfeng CUI Yinghui +1 位作者 FAN Wei PEI Shengwei 《Aerospace China》 2016年第3期36-43,共8页
The technological development status of new generation low cost small-lift launch vehicles applied to small satellite launch is investigated in this paper. The development trends are summarized, including low cost and... The technological development status of new generation low cost small-lift launch vehicles applied to small satellite launch is investigated in this paper. The development trends are summarized, including low cost and rapid response capability, utilization of mature rocket and missile technology, the development of mobile launch technology adopting air-based platforms and use of innovative technology. Moreover, the external power and internal demand of the small-lift launch vehicle are analyzed and the market prospect is forecasted. Finally, proposals for the development of small-lift launch vehicles are put forward, including exploration of the potential of existing rocket and missile technology, development of multi-platform mobile launch technology and further application of innovative technology and ideas. 展开更多
关键词 Small satellite Low cost Small-lift launch vehicle Development trends Market prospect
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