The Sunrise Balloon-Borne Stratospheric Solar Observatory, Peter Barthol

Автор: Phillip Chamberlin; William Dean Pesnell; Barbara
Название: The Solar Dynamics Observatory
ISBN: 1489992294 ISBN-13(EAN): 9781489992291
Издательство: Springer
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Описание: This volume is dedicated to the Solar Dynamics Observatory (SDO), which was launched 11 February 2010. Articles within also describe calibration results and data processing pipelines that are critical to understanding the data and products, concluding with a description of the successful Education and Public Outreach activities.

Автор: George Heald; John McKean; Roberto Pizzo
Название: Low Frequency Radio Astronomy and the LOFAR Observatory
ISBN: 3319234331 ISBN-13(EAN): 9783319234335
Издательство: Springer
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Описание: This book presents lecture materials from the Third LOFAR Data School, transformed into a coherent and complete reference book describing the LOFAR design, along with descriptions of primary science cases, data processing techniques, and recipes for data handling.

Автор: Peter J. Quinn; Krzysztof M. G?rski
Название: Toward an International Virtual Observatory
ISBN: 3662308177 ISBN-13(EAN): 9783662308172
Издательство: Springer
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Описание: The book is the first thorough overview of the first important steps to develop a worldwide virtual observatory so that, in the future, it could be easier to "dial-up" a part of the sky than wait many months to access a telescope.

Автор: Hannes Stephan Griebel
Название: Reaching High Altitudes on Mars With an Inflatable Hypersonic Drag Balloon
ISBN: 3834814253 ISBN-13(EAN): 9783834814258
Издательство: Springer
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Описание: Tbe main purpose of this work was to find a way of placing a meaningful scientific payload within the upper atmosphere of Mars such that certain scientific measurements become possible. So the altitude range covered and the possible dweIl time are relevant design drivers and will be explored in greater detail within this thesis. Either concept of flying on Mars, however, be it heavier or lighter than air (read: heavier or lighter than carbon dioxide) is restricted to altitodes weil below 10 km. Since any sustained light at that altitode or higher in such a thin atmosphere is teehnically impractical, so is ascending to that altitode with - sounding rocket. Therefore - team of scientists from several research institutes around Europe fonned a scientific committec. Together with engineers and scientists from tbe Mars Society Germany and tbe University ofthe Federal Armed Forces of Germany in Munich (UBW) the committee drafted a reference scientific mission scenario 1] to: find ways to da exactly that: providing an instrument suite with access to a large altitu. de range and. meaningful dwell time (see 10. 3. 1 starting onp. ge 208). Tbc most practical approach was found in an inflatable entry vehicle that can provide the largest and lightest possible configuration. Since 00 such attempts have yet been m. ade, the work described herein focuses mostly on the mathematical thcory and the technical peculiarities of such a system, but also treats mission design and testing aspects. 1.