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Titlebook: Astronautics; The Physics of Space Ulrich Walter Textbook 20183rd edition Springer Nature Switzerland AG 2018 Orbit mechanics.Orbit perturb

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發(fā)表于 2025-3-21 16:15:10 | 只看該作者 |倒序?yàn)g覽 |閱讀模式
期刊全稱Astronautics
期刊簡稱The Physics of Space
影響因子2023Ulrich Walter
視頻videohttp://file.papertrans.cn/164/163584/163584.mp4
發(fā)行地址The only textbook on the market dealing comprehensively with the physics of spaceflight.Based on the author‘s extensive teaching and his work with students.Provides problems and solutions covered in n
圖書封面Titlebook: Astronautics; The Physics of Space Ulrich Walter Textbook 20183rd edition Springer Nature Switzerland AG 2018 Orbit mechanics.Orbit perturb
影響因子.This introductory text covers all the key concepts, relationships, and ideas behind spaceflight and is the perfect companion for students pursuing courses on or related to astronautics. As a crew member of the STS-55 Space Shuttle mission and a full professor of astronautics at the Technical University of Munich, Ulrich Walter is an acknowledged expert in the field. This book is based on his extensive teaching and work with students, and the text is backed up by numerous examples drawn from his own experience. With its end-of-chapter examples and problems, this work is suitable for graduate level or even undergraduate courses in spaceflight, as well as for professionals working in the space industry. This third edition includes substantial revisions of several sections to extend their coverage. These include both theoretical extensions such as the study of relative motion in near-circular orbits, and more practical matters such as additional details about jet-engine and general rocket performance. New sections address regularized equations of orbital motion and their algebraic solutions and also state vector propagation; two new chapters are devoted to orbit geometry and orbit det
Pindex Textbook 20183rd edition
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Eine neue Definition des Leistungsfaktors,brium with its space environment. Knowing these inside temperatures is essential when designing a S/C, as most components only work reliably within certain temperature ranges: batteries lose capacity and propellants may freeze.
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,Forschung und Prüfung als Grundaufgaben,elerate the propellant mass in the combustion chamber. Rather acceleration is achieved by accelerating ions in an electric field, the energy of which needs to be provided externally by an electric current source. This is both an advantage and a disadvantage at the same time. The advantage is that, t
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https://doi.org/10.1007/978-3-663-15996-4ssion to the planets in our solar system. Before we investigate the rocket’s motion in interplanetary space, it first has to ascent in Earth’s gravitational field through the atmosphere. As will be shown later, ascent and reentry are subject to identical physical laws treated by the science called .
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,über Anwendungen der Elektronenbeugung,to be a concrete realization of a conceptional . with a choice of a .—meaning: a system of coordinates, such as rectangular (Cartesian), polar, or cylindrical coordinates, adapted to the symmetry of the problem—having a specific origin and orientation. (Note that “reference frame” and “coordinate sy
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