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921.
Jiang Dongsheng Bu Xueqin Sun Bing Lin Guiping Zhao Hongtao Cai Yan Fang Ling 《中国航空学报》2016,(4):863-873
The ceramic membrane oxygen generation technology has advantages of high concentra-tion of produced oxygen and potential nuclear and biochemical protection capability. The present paper studies the ceramic membrane technology for onboard oxygen generation. Comparisons are made to have knowledge of the effects of two kinds of ceramic membrane separation technologies on oxygen generation, namely electricity driven ceramic membrane separation oxygen generation technology (EDCMSOGT) and pressure driven ceramic membrane separation oxygen generation technology (PDCMSOGT). Experiments were conducted under different temperatures, pressures of feed air and produced oxygen flow rates. On the basis of these experiments, the flow rate of feed air, electric power provided, oxygen recovery rate and concentration of produced oxygen are compared under each working condition. It is concluded that the EDCMSOGT is the oxygen generation means more suitable for onboard conditions. 相似文献
922.
InSight Mars Lander Robotics Instrument Deployment System 总被引:1,自引:0,他引:1
A. Trebi-Ollennu Won Kim Khaled Ali Omair Khan Cristina Sorice Philip Bailey Jeffrey Umland Robert Bonitz Constance Ciarleglio Jennifer Knight Nicolas Haddad Kerry Klein Scott Nowak Daniel Klein Nicholas Onufer Kenneth Glazebrook Brad Kobeissi Enrique Baez Felix Sarkissian Menooa Badalian Hallie Abarca Robert G. Deen Jeng Yen Steven Myint Justin Maki Ali Pourangi Jonathan Grinblat Brian Bone Noah Warner Jaime Singer Joan Ervin Justin Lin 《Space Science Reviews》2018,214(5):93
The InSight Mars Lander is equipped with an Instrument Deployment System (IDS) and science payload with accompanying auxiliary peripherals mounted on the Lander. The InSight science payload includes a seismometer (SEIS) and Wind and Thermal Shield (WTS), heat flow probe (Heat Flow and Physical Properties Package, HP3) and a precision tracking system (RISE) to measure the size and state of the core, mantle and crust of Mars. The InSight flight system is a close copy of the Mars Phoenix Lander and comprises a Lander, cruise stage, heatshield and backshell. The IDS comprises an Instrument Deployment Arm (IDA), scoop, five finger “claw” grapple, motor controller, arm-mounted Instrument Deployment Camera (IDC), lander-mounted Instrument Context Camera (ICC), and control software. IDS is responsible for the first precision robotic instrument placement and release of SEIS and HP3 on a planetary surface that will enable scientists to perform the first comprehensive surface-based geophysical investigation of Mars’ interior structure. This paper describes the design and operations of the Instrument Deployment Systems (IDS), a critical subsystem of the InSight Mars Lander necessary to achieve the primary scientific goals of the mission including robotic arm geology and physical properties (soil mechanics) investigations at the Landing site. In addition, we present test results of flight IDS Verification and Validation activities including thermal characterization and InSight 2017 Assembly, Test, and Launch Operations (ATLO), Deployment Scenario Test at Lockheed Martin, Denver, where all the flight payloads were successfully deployed with a balloon gravity offload fixture to compensate for Mars to Earth gravity. 相似文献
923.
在美育教育教学过程中提高学生的美术意识,是培养具有创新意识和创新能力的新型美术人才的关键环节,在美育教育过程中,通过改善教学条件与教学手段,促进学生的创新意识以及利用现代科学技术等措施来提高学生的意识水平。 相似文献
924.
杨琳 《西安航空技术高等专科学校学报》2008,26(2):11-13
为了弥补在文学语言中的不足,形成了以象寓意的话语蕴藉现象。本文运用了列举、分析等方式诠释话语蕴藉与文学词语、文学修辞、标点符号及文章结构之间的联系,揭示出文学话语蕴藉带给读者的丰富想象和再创造的审美空间。 相似文献
925.
926.
六点炉温追踪仪(BYKO-TRACK)能准确、科学的测试各种不同结构烘房的温度曲线。本文介绍了该仪器在烘房的工艺设计、工件烘烤质量及涂料选材等方面的应用。 相似文献
927.
928.
飞机燃油密度高精度的测量对精确控制燃油量有重要作用.本文通过理论分析及ANSYS有限元分析软件对谐振式燃油密度传感器振动筒进行了振动模态分析,并利用正交实验设计法优化了不同振动模态、不同振动频率下振动筒的设计.分析结果表明:采用基本振型m=1,n=4,几何尺寸为L=2.9 cm,R=0.8 cm,t=0.20 mm的振动筒时,在密度范围为700~900 kg/m3的航空煤油环境下,其谐振频率范围为7.5~8.5 kHz.符合设计目标频率在2~10 kHz的要求,可作为谐振式燃油密度测量系统振动筒的设计参考. 相似文献
929.
Lin Li 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008
Retrieval of lunar soil composition is commonly achieved through optical remote sensing in which spectral characteristics of returned lunar samples are related to their constituents. Partial least squares (PLS) and principal component regression (PCR) were applied to the dataset characterized by the Lunar Soil Characterization Consortium (LSCC) to estimate the content of FeO, Al2O3 and TiO2 in the soils. The goal of this study was to test whether the conversion of reflectance to single scattering albedo (SSA) via Hapke’s radiative transfer model is able to improve the performance of PLS and PCR. Results from PLS and PCR modeling of SSA spectra indicate that the conversion does not necessarily improve the performance of PLS and PCR, and this depends on the chemical considered, the way to select the number of optimal factors, and how the data were pretreated. The conversion failed to accommodate the large deviation of highland samples with low FeO, TiO2 and high Al2O3. 相似文献
930.
捷联惯组历次测试数据反映了捷联惯组的逐次通电稳定性,它是引起制导工具误差的主要影响因素。本文采用建立捷联惯组历次测试数据灰色模型的方法对其逐次通电稳定性的变化趋势进行预测。通过仿真计算,验证了利用该方法进行短期预测的有效性。 相似文献