全文获取类型
收费全文 | 340篇 |
免费 | 99篇 |
国内免费 | 48篇 |
专业分类
航空 | 300篇 |
航天技术 | 89篇 |
综合类 | 31篇 |
航天 | 67篇 |
出版年
2024年 | 2篇 |
2023年 | 9篇 |
2022年 | 15篇 |
2021年 | 19篇 |
2020年 | 27篇 |
2019年 | 19篇 |
2018年 | 26篇 |
2017年 | 23篇 |
2016年 | 17篇 |
2015年 | 14篇 |
2014年 | 20篇 |
2013年 | 19篇 |
2012年 | 21篇 |
2011年 | 28篇 |
2010年 | 20篇 |
2009年 | 26篇 |
2008年 | 22篇 |
2007年 | 28篇 |
2006年 | 25篇 |
2005年 | 18篇 |
2004年 | 13篇 |
2003年 | 13篇 |
2002年 | 12篇 |
2001年 | 10篇 |
2000年 | 15篇 |
1999年 | 4篇 |
1998年 | 3篇 |
1997年 | 3篇 |
1996年 | 2篇 |
1995年 | 4篇 |
1994年 | 1篇 |
1993年 | 1篇 |
1992年 | 3篇 |
1991年 | 1篇 |
1990年 | 1篇 |
1989年 | 1篇 |
1984年 | 2篇 |
排序方式: 共有487条查询结果,搜索用时 15 毫秒
201.
202.
Oleg Polovnikov 《Aerospace Science and Technology》2000,4(8):567
At present, various radio navigation systems are employed during the automated approach of a transport vehicle to a space station. Experience has shown that emergency situations can occur in which it is necessary to revert to manual override of the automatic approach.Such situations have indeed occurred during flight operations of the space station Mir. The crews of the transport vehicles and the Mir used manual steering more than 30 times for successful docking, and four times for approach to the station.Successful manual steering demands absolute understanding of the relative orbit parameters. The decisive task of the crew is to determine these relative parameters. This is possible using visual observations from either the transport vehicle or the station using simple and reliable instruments. This article explains the algorithm for determining the relative orbits from visual crew observations, based on similarities of relative orbit families. 相似文献
203.
用拦格朗日乘子法,利用向量分析的工具及巧妙的变换,对带磨擦约束的弹塑性接触问题的变分不等原理进行了严格的证明。 相似文献
204.
205.
刘景旺 《华北航天工业学院学报》2007,(1)
本文报导了通过结合自行制备的掺铈钒酸钇晶体(Ce3 :YVO4)荧光粉与InGaN/GaN蓝光发光二极管(LED)结合而得的白光发光二极管(W-LED)。在室温、正向电压3.5V、正向电流20mA时W-LED的CIE色坐标为(0.32,0.37),接近纯白色(0.33,0.33)。 相似文献
206.
针对相对疏松的铸造钛合金和相对密实的锻造钛合金的焊接问题,开展了两种状态的TC4钛合金电子束焊接工艺研究,对比了不同焊接参数对焊接质量的影响。研究结果表明,采用方波扫描可以较好地实现铸造钛合金与锻造钛合金的连接,焊缝成形良好,内部无缺陷;焊接接头力学性能分析表明,拉伸断裂位置全部在铸件母材区一侧。实焊结果证明,电子束焊接可以实现异种状态TC4钛合金焊接的工程化应用。 相似文献
207.
In 2012 we celebrate the 70th anniversary of the first successful rocket launch that reached a height of 84.5 km and had a speed of 4.824 km/h (5x sonic speed). This rocket flew 190 km to the target location. One of the masterminds of this launch was Walter Thiel, a German chemist and rocket engineer. Thiel was highly talented, during his education from primary school until diploma exams he always received a grade of A in his exams. He was called “the student with the 7 A grades”. In 1934 Thiel became Dr.-Ing. (chem.), with the highest possible honor (summa cum laude), when he was only 24 years old. He started to work for the rocket development department at Humboldt University, Berlin. Walter Dornberger asked him to leave the university research department and become head of rocket propulsion development in his team in Kummersdorf, near Berlin. Thiel's groundbreaking ideas for the rocket engine would lead to a significant reduction in material, weight and work processes, as well as a shortening in the length of the engine itself. Thiel and his team also defined the fuel itself and the best ratio of mixture between ethanol and liquid oxygen for the engine. In 1940 the propulsion team moved from Kummersdorf to Peenemünde after the launch sites were completed there. Thiel became deputy of Wernher von Braun at the R&D units. One of Thiel's team members was Konrad Dannenberg, who later became famous in the development of the Saturn program. On the night from August 17 to August 18, 1943, Thiel and his family (wife and two children) were killed during a Royal Air Force bombing raid (Operation Hydra). The Moon crater “Thiel” on the far side of the Moon is named after Walter Thiel. The research results of Walter Thiel had a strong impact on the United States' rocket program as well as the Russian rocket development program. 相似文献
208.
Simulation of asymmetric landing and typical ground maneuvers for large transport aircraft 总被引:6,自引:0,他引:6
Prashant Dilip Khapane 《Aerospace Science and Technology》2003,7(8):1708-619
It is important to determine static and dynamic ground loads for the aircraft ground maneuvers accurately in the design phase. Simulation of the important operational cases is a better way compared to the tests on real aircraft to investigate these loads at a reasonable cost. In this paper, the simulation of an asymmetric landing case and typical ground maneuvers for large transport aircraft is presented. The aircraft models are built in the multibody simulation tool SIMPACK. The tire model implemented in SIMPACK includes lateral dynamics of the tire. Cornering, braked runs and pushback are simulated as typical ground maneuvers. For simulation of braking, a simple but effective Antilock Braking System (ABS) algorithm is implemented. The article is based on the work done in cooperation between DLR and Airbus in the Flexible Aircraft 2 project. 相似文献
209.
美国空军信息作战初探 总被引:3,自引:0,他引:3
在信息战条件下 ,美空军正大力发展全球定位系统 (GPS) ,充分利用C4ISR(指挥、控制、通信、计算机与情报、监视、侦察 )系统 ,关注信息网络和信息系统的安全 ,以提升空中平台的作战能力 ,最大限度地发挥武器系统及传统EW的效能 相似文献
210.