全文获取类型
收费全文 | 184篇 |
免费 | 185篇 |
国内免费 | 31篇 |
专业分类
航空 | 281篇 |
航天技术 | 43篇 |
综合类 | 19篇 |
航天 | 57篇 |
出版年
2024年 | 2篇 |
2023年 | 12篇 |
2022年 | 16篇 |
2021年 | 12篇 |
2020年 | 5篇 |
2019年 | 22篇 |
2018年 | 20篇 |
2017年 | 15篇 |
2016年 | 12篇 |
2015年 | 13篇 |
2014年 | 11篇 |
2013年 | 17篇 |
2012年 | 20篇 |
2011年 | 19篇 |
2010年 | 18篇 |
2009年 | 16篇 |
2008年 | 7篇 |
2007年 | 25篇 |
2006年 | 20篇 |
2005年 | 8篇 |
2004年 | 11篇 |
2003年 | 12篇 |
2002年 | 6篇 |
2001年 | 10篇 |
2000年 | 19篇 |
1999年 | 3篇 |
1998年 | 14篇 |
1997年 | 5篇 |
1996年 | 4篇 |
1995年 | 7篇 |
1994年 | 2篇 |
1993年 | 4篇 |
1992年 | 2篇 |
1989年 | 1篇 |
1988年 | 2篇 |
1987年 | 8篇 |
排序方式: 共有400条查询结果,搜索用时 15 毫秒
71.
碳纤维复合材料卫星天线反射面型面精度稳定性分析 总被引:1,自引:0,他引:1
文章简述了卫星天线的组成、制造工艺过程,着重对影响天线反射面型面精度和尺寸稳定性有关内容,从材料特性、铺层分析、成型模具材料和产品质量控制等内容进行了分析。 相似文献
72.
文章介绍了北京空间机电研究所研制的某型号卫星碳 /环氧面板 -铝蜂窝夹层结构件结构特点及损伤情况 ,且对损伤修补内容作了较详细叙述 相似文献
73.
74.
燃烧室新材料在卫星双组元低推力发动机上的应用 总被引:5,自引:0,他引:5
对有代表性、有发展前途的几种新材料进行比较 ,并根据应用新材料的低推力发动机燃烧室的结构特点 ,分析了不同冷却方式对双组元低推力发动机性能损失的影响 ,为双组元低推力发动机燃烧室的材料选择、加工工艺、设计优化提供参考。 相似文献
75.
介绍了一种平均压缩率达到10%,平均压缩回弹率达到13%的低密度碳/碳材料及其独特的制造技术,对改善碳/碳材料的韧性提供了一种行之有效的方法。其主要工艺途径为,在水中以表面活性剂分散、包覆原材料、混合抽滤、烘干固化、炭化等工序。 相似文献
76.
《中国航空学报》2016,(2):411-423
This article examines the suitability of fabricating artificial, dragonfly-like, wing frames from materials that are commonly used in unmanned aircraft(balsa wood, black graphite carbon fiber and red prepreg fiberglass). Wing frames made with Type 321 stainless steel are also examined for comparison. The purpose of these wings is for future use in biomimetic micro aerial vehicles(BMAV). BMAV are a new class of unmanned micro-sized aerial vehicles that mimic flying biological organisms(like flying insects). Insects, such as dragonflies, possess corrugated and complex vein structures that are difficult to mimic. Simplified dragonfly-like wing frames were fabricated from these materials and then a nano-composite film was adhered to them, which mimics the membrane of an actual dragonfly. Finite element analysis simulations were also performed and compared to experimental results. The results showed good agreement(less than 10% difference for all cases).Analysis of these results shows that stainless steel is a poor choice for this wing configuration, primarily because of the aggressive oxidation observed. Steel, as well as balsa wood, also lacks flexibility. In comparison, black graphite carbon fiber and red prepreg fiberglass offer some structural advantages, making them more suitable for consideration in future BMAV applications. 相似文献
77.
《中国航空学报》2020,33(5):1541-1548
Uni-directional carbon/carbon composites with high thermal conductivity are suitable to supply continuous thermal protection for future reentry vehicles since they could reduce surface temperature and ablation rates simultaneously in harsh environments. In this work, the high thermal conductivity carbon/carbon composites were prepared by chemical vapor infiltration. After heat-treatment, both their open porosity and internal friction increase due to the fiber/matrix thermal expansion mismatch; while their thermal conductive performance become better due to more complete carbon structure. With raising heat-treatment temperature from 1800 °C to 2450 °C, the mass and linear ablation rates of C/C composites with fibers vertical to the oxyacetylene torch for 60 s decrease from 0.66 mg/s and 2.95 μm/s to 0.51 mg/s and 2.05 μm/s respectively. The improved ablation resistance is resulted from the increased thermal conductivity from 282 to 508 W/(m·K) and more carbon fibers exposed to the flame during ablation, which have better oxidation resistance than those of carbon matrix. While such ablation rates become larger for composites with fibers parallel to the flame, from 1.02 mg/s and 3.73 μm/s to 1.28 mg/s and 5.01 μm/s respectively since the ablation occurred more easily through gaps at the fiber/matrix interfaces, which become larger and are always exposed to the flame for this case. 相似文献
78.
Soil carbon distribution and site characteristics in hyper-arid soils of the Atacama Desert: A site with Mars-like soils 总被引:1,自引:0,他引:1
Julio E. Valdivia-Silva Rafael Navarro-González Lauren Fletcher Saúl Perez-Montaño Reneé Condori-Apaza Christopher P. Mckay 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012
The soil carbon content and its relation to site characteristics are important in evaluating current local, regional, and global soil C storage and projecting future variations in response to climate change. In this study we analyzed the concentration of organic and inorganic carbon and their relationship with in situ climatic and geological characteristics in 485 samples of surface soil and 17 pits from the hyper-arid area and 51 samples with 2 pits from the arid–semiarid region from the Atacama Desert located in Peru and Chile. The soil organic carbon (SOC) in hyperarid soils ranged from 1.8 to 50.9 μg C per g of soil for the 0–0.1 m profile and from 1.8 to 125.2 μg C per g of soil for the 0–1 m profile. The analysis of climatic (temperature and precipitation), elevation, and some geologic characteristics (landforms) associated with hyper-arid soils explained partially the SOC variability. On the other hand, soil inorganic carbon (SIC) contents, in the form of carbonates, ranged from 200 to 1500 μg C per g of soil for the 0–0.1 m profile and from 200 to 3000 μg C per g of soil for the 0–1.0 m profile in the driest area. The largest accumulations of organic and inorganic carbon were found near to arid–semiarid areas. In addition, the elemental carbon concentrations show that the presence of other forms of inorganic carbon (e.g. graphite, etc.) was negligible in these hyperarid soils. Overall, the top 1 m soil layer of hyperarid lands contains ∼11.6 Tg of organic carbon and 344.6 Tg of carbonate carbon. The total stored carbon was 30.8-fold the organic carbon alone. To our knowledge, this is the first study evaluating the total budget carbon on the surface and shallow subsurface on ∼160,000 km2 of hyperarid soils. 相似文献
79.
AZ91镁合金负压消失模铸造充型速度的研究 总被引:9,自引:0,他引:9
真空度、浇注温度及模样厚度对AZ91镁合金消失模铸造充型速度影响的全因子实验的结果表明 ,它们都对充型速度起积极的作用 ,真空度是决定充型速度的一个关键工艺参数。在不抽真空时 ,充型速度非常小且随充型过程的进行逐渐降低 ,浇注温度对充型速度的影响也很小 ;抽真空时 ,充型速度在充型过程中不断变化且呈现不出任何规律 ,其起伏的幅度随真空度、浇注温度和模样厚度的增大而增大 ;在真空度较低时 ,随着真空度和 或浇注温度的提高 ,平均充型速度迅速增大 ,真空度与浇注温度对充型速度的交互作用增强 ;在较高的真空度下 ,平均充型速度仍随浇注温度的提高而增大 ,但平均充型速度的增大速率却随真空度的进一步提高而降低 ,真空度与浇注温度对充型速度的交互作用很弱。模样厚度对平均充型速度影响在抽真空时有所提高。 相似文献
80.