Titlebook: Reaching High Altitudes on Mars With an Inflatable Hypersonic Drag Balloon; Hannes Griebel Book 2010 Vieweg+Teubner Verlag | Springer Fach

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Hannes Griebeland research, including an examination of the evolution of internal control theory..The author presents detailed perspectives on the elements of management control systems and introduces masterful new ideas and978-3-662-52340-7978-3-642-54715-7Series ISSN 2196-3134 Series E-ISSN 2196-3142

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Related Technologies and State of the Art,gap in the accessible measurement range: That of the intermediate scale. That of long range mobility of planetary dimensions combined with in-situ atmosphere measurements and birds-eye perspective imaging. A very good overview of past concepts, actual attempts and future plans for planetary areal re

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Flight Dynamics Analysis,IMEDES Hypersonic Flight and Low speed descent. ARCHYFLOW analyses were performed starting with 3D trajectory simulations [39], including steady state [40] and transient [41] thermal analyses. Critical points along the hypersonic flight trajectory were further studied in in detail using CFD analyses

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Material Analysis, temperature differences during hypersonic flight, yet be light enough for a reasonable mission, it has to be made of a high performance thin-film material or a laminate thereof. Such materials are tested as part of project ARCHIMATTER, which stands for ARCHIMEDES Material Testing and Research. It i

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Transportation and Deployment System,ft‘s point of release. During interplanetary cruise, the ballute has to be kept well tempered and prevented from cold welding of packed envelope layers. Upon deployment, the system has to ensure that the ballute spacecraft properly unfolds in space and is held in position until fully inflated. Event

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Mission and Spacecraft Design for Ballute Applications,t on mission design and vice versa. This is true even when compared to ordinary entry vehicles, because the deceleration altitude itself is of no concern, so long as no one gets hurt, and because relatively dense and small vehicles can tolerate a larger variation in the ballistic coefficient with co

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Conclusion and Outlook, body (referred to as “ballute”) that is able to withstand the mechanical and heating loads during atmospheric entry. It could also be shown that a high performance ballute may be used to achieve a certain scientific goal by reaching altitudes otherwise inaccessible (which is a new concept introduce

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Related Technologies and State of the Art,osphere measurements and birds-eye perspective imaging. A very good overview of past concepts, actual attempts and future plans for planetary areal reconnaissance missions can be found in reference [7].