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文章对国内外航天器热控涂层在轨搭载飞行试验进行了调研,综述了利用和平号空间站、"国际空间站"、美国航天飞机、"长期暴露装置"等航天器进行的相关试验工作及主要的研究成果等。在此基础上提出了我国开展热控涂层搭载飞行试验的建议。 相似文献
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Gioia D. Massa Cary A. Mitchell 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012
Sweetpotato (Ipomea batatas L.) ‘Whatley–Loretan’ was developed for space life support by researchers at Tuskegee University for its highly productive, nutritious storage roots. This promising candidate space life-support crop has a sprawling habit and aggressive growth rate in favorable environments that demands substantial growing area. Shoot pruning is not a viable option for vine control because removal of the main shoot apex drastically inhibits storage-root initiation and development, and chemical growth retardants typically are not cleared for use with food crops. As part of a large effort by the NASA Specialized Center of Research and Training in Advanced Life Support to reduce equivalent system mass (ESM) for food production in space, the dilemma of vine management for sweetpotato was addressed in effort to conserve growth area without compromising root yield. Root yields from unbranched vines trained spirally around wire frames configured either in the shapes of cones or cylinders were similar to those from vines trained horizontally along the bench, but occupying only a small fraction of the bench area. This finding indicates that sweetpotato is highly adaptable to a variety of vine-training architectures. Planting a second plant in the growth container and training the two vines in opposite directions around frames enhanced root yield and number, but had little effect on average length of each vine or bench area occupied. Once again, root yields were similar for both configurations of wire support frames. The 3–4-month crop-production cycles for sweetpotato in the greenhouse spanned all seasons of multiple years during the course of the study, and although electric lighting was used for photoperiod control and to supplement photosynthetic light during low-light seasons, there still were differences in total light available across seasons. Light variations and other environmental differences among experiments in the greenhouse had more effects on vine length than on root yield. Average vine length correlated positively with total hours of daylight received across seasons, and responses for one plant per container were higher above a threshold duration of solar exposure, suggesting that the vines of two plants per container compete for available light. In addition to the adaptability of sweetpotato to various vine-training architectures and across seasons in terms of maintaining root productivity, the open, interior volumes of the support frames tested in this study will provide future opportunity to enhance sweetpotato root yield in space by adding novel interior lighting, such as from intracanopy arrays of light-emitting diodes. This work was sponsored by NASA grant NAG 5 1286. 相似文献
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雷春仪 《中国民航飞行学院学报》2013,24(4):68-71
本文阐述了基于以网络输出为导向的任务型教学模式的基本定义、特点,教学步骤和设计理念。通过讨论此教学模式在大学英语听说教学中的应用,总结和反思教学实践,证明基于网络环境下以输出为导向的任务型教学是一种行之有效的教学模式,能切实有效地优化英语听说课堂教学。 相似文献
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针对固液动力探空火箭在进行测试、飞行试验时,需要实时测量并记录推力、燃料供给速率以及吹除系统工况信息的问题,设计并工程实现了对箭载重要设备输出信号进行监控和采集记录的数据采集系统.以STM32F103RB微控制器为核心,完成了数据采集、存储、传输等电路的设计,并在Real View MDK集成开发环境下,运用C语言完成了控制、测试程序的编写.最后,通过Real View ULINKR仿真器实现了软硬件的联合测试,验证了系统的供电控制、采样频率、工况记录等功能都满足设计要求,完成了对箭载重要设备监控和采集记录的任务.只需修改微控制器内的操控程序,就可将此数据采集系统应用于不同型号的固液动力探空火箭. 相似文献
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防隔热/承载一体化热防护的结构承载功能使其比传统热防护具有更高的结构效率。近年来,已经发展了波纹夹芯一体化热防护及改进方案、刚性隔热夹芯一体化热防护、多层级一体化热防护等多种一体化热防护概念。首先介绍了各方案的结构特征,分析了各方案的热短路效应和结构承载性能。阐述了一体化热防护等效性能分析与热力耦合响应高效分析方法。介绍了热力耦合约束下一体化热防护的结构尺寸优化与材料优选方法。论述了一体化热防护非确定性分析与设计方面的研究进展。在此基础上,总结了一体化热防护发展的特点和不足,探讨了一体化热防护的发展方向。 相似文献
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