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251.
据美国全球安全网2010年12月13日报道,美国已成功完成首颗"天基红外系统"地球静止轨道卫星的最终集成系统测试,该卫星将于2011年春天用宇宙神-5火箭从卡纳维拉尔角空军基地发射,它将显著提升美国的导弹预警能力和对其他重要国家安全任务的同步支持能力,包括导弹防御、技术情报和战场太空感知。 相似文献
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6月13日,日本宇宙探索局的“隼鸟”号小行星探测器再入大气层,降落在澳大利亚南部伍麦拉附近的沙漠地带,时隔7年后回归地球。期间,多灾多难,百折不挠,“隼鸟”由此也博得“不死鸟”的尊称。 相似文献
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Ebert Franz-Josef 《中国航空学报》2007,20(4):378-384
In this paper, the operating conditions, technical requirements, performance characteristics, design ideas, application experiences and development trends of aerospace engine bearings, including material technology, integration design and reliability, are reviewed. The development history of aerospace engine bearing is recalled briefly at first. Then today's material technologies and the high bearing performances of the bearings obtained through the new materials are introduced, which play important roils in the aeroengine bearing developments. The integration design ideas and practices are explained to indicate its significant advantages and importance to the aerospace engine bearings. And the reliability of the shaft-bearing system is pointed out and treated as the key requirement with goals for both engine and bearing. Finally, as it is believed that the correct design comes from practice, the pre-qualification rig testing conducted by FAG Aerospace GmbH & Co. KG is briefly illustrated as an example. All these lead to the development trends of aerospace engine bearings from different aspects. 相似文献
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Wan Dawei Guo Rongwei 《中国航空学报》2007,20(4):304-312
A fixed-geometry two-dimensional mixed-compression supersonic inlet with sweep-forward high-light and bleed slot in an inverted "X"-form layout was tested in a wind tunnel. Results indicate: (1) with increases of the free stream Mach number, the total pressure recovery decreases, while the mass flow ratio increases to the maximum at the design point and then decreases; (2) when the angle of attack, a, is less than 6°, the total pressure recovery of both side inlets tends to decrease, but, on the lee side inlet, its values are higher than those on the windward side inlet, and the mass flow ratio on lee side inlet increases first and then falls, while on the windward side it keeps declining slowly with the sum of mass flow on both sides remaining almost constant; (3) with the attack angle, a, rising from 6° to 9°, both total pressure recovery and mass flow ratio on the lee side inlet fall quickly, but on the windward side inlet can be observed decreases in the total pressure recovery and increases in the mass flow ratio; (4) by comparing the velocity and back pressure characterristics of the inlet with a bleed slot to those of the inlet without, it stands to reason that the existence of a bleed slot has not only widened the steady working range of inlet, but also made an enormous improvement in its performance at high Mach numbers. Besides, this paper also presents an example to show how this type of inlet is designed. 相似文献
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