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Linearly combined transition model based on empirical spot growth correlations 基于实证现货增长相关性的线性组合过渡模型
IF 1.4 Q2 ENGINEERING, AEROSPACE Pub Date : 2023-05-09 DOI: 10.1007/s12567-023-00499-8
Maximilian Karsch, J. Van den Eynde, J. Steelant
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引用次数: 0
Mission design for point-to-point passenger transport with reusable launch vehicles 用可重复使用的运载火箭进行点对点客运的任务设计
IF 1.4 Q2 ENGINEERING, AEROSPACE Pub Date : 2023-05-06 DOI: 10.1007/s12567-023-00498-9
Jascha Wilken, Steffen Callsen
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引用次数: 2
Hybrid adaptive sliding mode attitude control for earth pointing nanosatellites 指向地球的纳米卫星的混合自适应滑模姿态控制
IF 1.4 Q2 ENGINEERING, AEROSPACE Pub Date : 2023-04-29 DOI: 10.1007/s12567-023-00490-3
Ilyas El wafi, M. Haloua, Z. Guennoun, Zakaria Moudden
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引用次数: 0
A novel antenna steering mechanism with self hold-down feature for communication spacecrafts 一种新型通信航天器天线自保持转向机构
IF 1.4 Q2 ENGINEERING, AEROSPACE Pub Date : 2023-04-21 DOI: 10.1007/s12567-023-00496-x
A. Kapoor, B. Nagaraj, Abhishek Kumar, H. N. Kumar, B. V. S. Dinesh, N. Viswanatha, D. M. Reddy, Sidharth Tiwary, A. Shankara, K. Prakasha, B. K. Muthu
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引用次数: 0
Hyplane: a single-stage suborbital aerospaceplane. 超级飞机:单级亚轨道航空航天飞机。
IF 1.4 Q2 ENGINEERING, AEROSPACE Pub Date : 2023-04-15 DOI: 10.1007/s12567-023-00494-z
Gennaro Russo, Claudio Voto

This paper has the aim to report the status of the HYPLANE project to date. HYPLANE is a horizontal take-off and landing Mach 4.5 bizjet-size aerospaceplane conceived by Trans-Tech and University Federico II of Naples and under study within the industrial-academic ecosystem of the Campania Aerospace District (DAC). HYPLANE has the aim to offer very fast suborbital flight for space tourism, microgravity experimentation and training, and also shortening time to connect two distant airports within a door-to-door scenario. The concept is based on the access to stratospheric altitudes (30 km) for either point-to-point stratospheric or suborbital flights as safe as today's commercial air transportation, by integrating enhanced state-of-the-art aeronautical and space technologies. Essentially, HYPLANE is mostly based on already relatively high TRL technologies which guarantees a sufficiently short time to market. The low wing loading configuration and designed ability to manoeuvre along the flight trajectories at small angles of attack, allow HYPLANE to guarantee accelerations and load factors of the same order as those characterizing the present civil aviation aircraft (FAA/EASA specifications). Thanks to its technical features, it may operate from/to more than 5000 airports all over the world needing short runways to take-off and land, which for point-to-point business aviation is paramount. Furthermore, characteristics such as small dimension, configuration and high cruising altitude determine reduced noise in the airports surrounding and low sonic boom impact on ground. These conditions will further facilitate not only the development of the commercial use of such kind of transportation mean, but also its social acceptability.

本文旨在报告HYPLANE项目的现状。HYPLANE是一种水平起降速度为4.5马赫的商务喷气机大小的航空航天飞机,由Trans-Tech和那不勒斯费德里科二世大学共同设计,目前正在坎帕尼亚航空航天区(DAC)的工业-学术生态系统中进行研究。HYPLANE的目标是为太空旅游、微重力实验和训练提供非常快的亚轨道飞行,并在门到门的情况下缩短连接两个遥远机场的时间。这个概念是基于进入平流层高度(30公里),无论是点对点的平流层飞行还是亚轨道飞行,都像今天的商业航空运输一样安全,通过整合最先进的航空和空间技术。从本质上讲,HYPLANE主要基于已经相对较高的TRL技术,这保证了足够短的上市时间。低翼载荷配置和设计的能力,沿飞行轨迹在小迎角机动,允许HYPLANE保证加速度和载荷系数相同的顺序,那些特征的民用航空飞机(FAA/EASA规范)。由于其技术特点,它可以在全球5000多个需要短跑道起降的机场之间运行,这对于点对点商务航空来说是至关重要的。此外,小尺寸、结构和高巡航高度等特点决定了其在机场周边的噪声降低和对地面的低音爆冲击。这些条件不仅会进一步促进这种交通工具商业用途的发展,而且会进一步促进其社会可接受性。
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引用次数: 1
Characterization of polyethylene terephthalate (PET) materials under high-energy electron exposure 高能电子暴露下聚对苯二甲酸乙二醇酯(PET)材料的表征
IF 1.4 Q2 ENGINEERING, AEROSPACE Pub Date : 2023-04-12 DOI: 10.1007/s12567-023-00495-y
J. Shah, M. Bengtson, Sydney Collman, R. Hoffmann, D. Ferguson, D. Engelhart, E. Plis
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引用次数: 1
Precise in-orbit relative navigation technique for rendezvous mission of CubeSats using only GPS receivers 仅使用GPS接收器的立方体卫星交会任务的精确在轨相对导航技术
IF 1.4 Q2 ENGINEERING, AEROSPACE Pub Date : 2023-04-08 DOI: 10.1007/s12567-023-00488-x
H. Shim, O. Kim, Sunkyoung Yu, C. Kee, D. Cho, Hae-Dong Kim
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引用次数: 0
Design and control of high voltage gain DC–DC converter for CubeSat propulsion 立方体卫星推进用高压增益DC-DC变换器的设计与控制
IF 1.4 Q2 ENGINEERING, AEROSPACE Pub Date : 2023-04-05 DOI: 10.1007/s12567-023-00493-0
Abdelaali Ouhammam, H. Mahmoudi, H. Ouadi
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引用次数: 0
Approximation models for drag and heat flux of random tumbling objects in the transitional regime 随机翻滚物体在过渡状态下的阻力和热通量的近似模型
IF 1.4 Q2 ENGINEERING, AEROSPACE Pub Date : 2023-04-03 DOI: 10.1007/s12567-023-00492-1
Pierre Van Hauwaert
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引用次数: 1
Investigation of X-band and Ka-band amplitude scintillation based on measurement data collected during ESA’s BepiColombo superior solar conjunction campaign 基于欧空局BepiColombo超日合观测收集的测量数据对x波段和ka波段振幅闪烁的研究
IF 1.4 Q2 ENGINEERING, AEROSPACE Pub Date : 2023-03-31 DOI: 10.1007/s12567-023-00491-2
Shunli Chen, M. Lanucara, J. Villalvilla
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引用次数: 0
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CEAS Space Journal
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