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Titlebook: ?ffentlichkeit – für alle?; Themen und Informati Matthias Begenat Book 2016 Springer Fachmedien Wiesbaden 2016 Politische Kommunikation.The

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21#
發(fā)表于 2025-3-25 03:23:27 | 只看該作者
22#
發(fā)表于 2025-3-25 09:31:43 | 只看該作者
https://doi.org/10.1007/978-3-662-21593-7er wahrgenommenen Transparenz, der wahrgenommenen Relevanz und der Interessenrepr?sentation werden dabei zun?chst pro politischem Milieu geprüft und lediglich für die Kontrastierung nebeneinander gestellt. Die Frage nach der gemeinsamen Agenda wird mittels eines Vergleichs der politischen Milieus beantwortet.
23#
發(fā)表于 2025-3-25 15:04:23 | 只看該作者
24#
發(fā)表于 2025-3-25 16:44:57 | 只看該作者
Biotic and abiotic stresses of pulse crops in Europebe effective in controlling biotic stresses, but several are not cost-efficient. Healthy seeds, seed treatment with chemicals, and the use of resistant and tolerant cultivars are now used to control several diseases. On the other hand, some constraints can only be controlled by avoiding infested soi
25#
發(fā)表于 2025-3-25 23:20:29 | 只看該作者
On Reducing the Impact of Interdomain Route Changes,ropped; after route convergence, changes in the egress point for reaching a destination can alter the network’s intradomain traffic patterns and trigger new traffic-engineering. In this paper, we look into reducing the impact of interdomain route changes on the network’s operation. First, we investi
26#
發(fā)表于 2025-3-26 00:23:23 | 只看該作者
MarCO: Interplanetary Mission Development on a CubeSat Scale its cruise phase, two CubeSats will deploy from the launch vehicle’s upper stage and begin independent flight to Mars (Fig. 1). During InSight’s entry, descent, and landing (EDL) sequence, these twin Mars Cube One (MarCO) spacecraft will fly 3500?km above the Martian surface, recording and relaying
27#
發(fā)表于 2025-3-26 06:32:20 | 只看該作者
28#
發(fā)表于 2025-3-26 11:01:58 | 只看該作者
Introduction to Space Flighth the same amount of propellant is introduced. Background material on the internal flow and combustion in chemical rockets is provided, in preparation for more detailed coverage of specific chemical systems in later chapters. Performance equations associated with the generation of thrust by a propulsive exhaust nozzle are presented.
29#
發(fā)表于 2025-3-26 15:33:33 | 只看該作者
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發(fā)表于 2025-3-26 18:49:51 | 只看該作者
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