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Kommentierung zu §§ 705-740
(2009)
Konvergenz von drahtlosen und drahtgebundenen Kommunikationstechnologien in der Gebäudeautomation
(2009)
Kraft-Wärme-Kälte-Kopplung im Leistungsbereich in 10kW mit periodisch arbeitender Sorptionsmaschine
(2009)
Layer-by-Layer Assembly of Carbon Nanotubes Incorporated in Light-Addressable Potentiometric Sensors
(2009)
Magnetotomography and Electric Currents in a Fuel Cell / Lustfeld, H. ; Reißel, M. ; Steffen, B.
(2009)
Microfabrication, characterization and analytical application of a new thin-film silver microsensor
(2009)
The so-called "compound solar sail", also known as "Solar Photon Thruster" (SPT), is a solar sail design concept, for which the two basic functions of the solar sail, namely light collection and thrust direction, are uncoupled. In this paper, we introduce a novel SPT concept, termed the Advanced Solar Photon Thruster (ASPT). This model does not suffer from the simplified assumptions that have been made for the analysis of compound solar sails in previous studies. We present the equations that describe the force, which acts on the ASPT. After a detailed design analysis, the performance of the ASPT with respect to the conventional flat solar sail (FSS) is investigated for three interplanetary mission scenarios: An Earth-Venus rendezvous, where the solar sail has to spiral towards the Sun, an Earth-Mars rendezvous, where the solar sail has to spiral away from the Sun, and an Earth-NEA rendezvous (to near-Earth asteroid 1996FG3), where a large orbital eccentricity change is required. The investigated solar sails have realistic near-term characteristic accelerations between 0.1 and 0.2mm/s2. Our results show that a SPT is not superior to the flat solar sail unless very idealistic assumptions are made.
Within ESA's Cosmic Vision 2015-2025 plan, a mission to explore the Saturnian System, with special emphasis on its two moons Titan and Enceladus, was selected for study, termed TANDEM (Titan and Enceladus Mission). In this paper, we describe an optimized mission design for a TANDEM-derived solar electric propulsion (SEP) mission. We have chosen the SEP mission scenario for the interplanetary transfer of the TANDEM spacecraft because all feasible gravity assist sequences for a chemical transfer between 2015 and 2025 result in long flight times of about nine years. Our SEP system is based on the German RIT ion engine. For our optimized mission design, we have extensively explored the SEP parameter space (specific impulse, thrust level, power level) and have calculated an optimal interplanetary trajectory for each setting. In contrast to the original TANDEM mission concept, which intends to use two launch vehicles and an all-chemical transfer, our SEP mission design requires only a single Ariane 5 ECA launch for the same payload mass. Without gravity assist, it yields a faster and more flexible transfer with a fight time of less than seven years, and an increased payload ratio. Our mission design proves thereby the capability of SEP even for missions into the outer solar system.
This study demonstrates the feasibility of applying free-breathing, cardiac-gated, susceptibility-weighted fast spin-echo imaging together with black blood preparation and navigator-gated respiratory motion compensation for anatomically accurate T₂ mapping of the heart. First, T₂ maps are presented for oil phantoms without and with respiratory motion emulation (T₂ = (22.1 ± 1.7) ms at 1.5 T and T₂ = (22.65 ± 0.89) ms at 3.0 T). T₂ relaxometry of a ferrofluid revealed relaxivities of R2 = (477.9 ± 17) mM⁻¹s⁻¹ and R2 = (449.6 ± 13) mM⁻¹s⁻¹ for UFLARE and multiecho gradient-echo imaging at 1.5 T. For inferoseptal myocardial regions mean T₂ values of 29.9 ± 6.6 ms (1.5 T) and 22.3 ± 4.8 ms (3.0 T) were estimated. For posterior myocardial areas close to the vena cava T₂-values of 24.0 ± 6.4 ms (1.5 T) and 15.4 ± 1.8 ms (3.0 T) were observed. The merits and limitations of the proposed approach are discussed and its implications for cardiac and vascular T₂-mapping are considered.
Next Generation Access Networks: Why is there a higher risk of investment and how to deal with it?
(2009)
Nitratfreie Molke
(2009)
Grasschnitt hat in Deutschland ein beträchtliches Potenzial als nachwachsender Rohstoff. Da frischer Grasschnitt nur in den Sommermonaten zur Verfügung steht und Gras bei der Lagerung verrottet, wird er unter anderem durch Silierung konserviert. Während der Silierung wird ein Teil der wasserlöslichen Kohlenhydrate unter anaeroben Bedingungen zu Milchsäure fermentiert. Die Kombination aus Luftabschluss und Ansäuerung bewirkt die Konservierung der Silage. Silage als weit verbreitetes landwirtschaftliches Erzeugnis ist somit ein potentieller, in großen Mengen verfügbarer Lieferant für eine Vielzahl von Substraten für mikrobielle Fermentationen. Diese können entweder durch die Hydrolyse der in den Pflanzen enthaltenen Cellulosen und Hemicellulosen oder durch die Verwendung eines Silagepresssaftes nutzbar gemacht werden. Die zu entwickelnden Prozesse sollen die verbleibenden Kohlenhydrate, inklusive der Cellulose und Hemicellulose, sowie die Milchsäure nutzen. Die in der Silage enthaltenen Zucker sollen zu Ethanol, Itakonsäure und Bernsteinsäure und die Milchsäure zu 1,2-Propandiol umgesetzt werden. Anfallende Reststoffe wie Hydrolyserückstände, Presskuchen und Fermentationsrückstände sollen bei allen zu etablierenden Prozessen entweder als Viehfutter verwendet oder der Biogasproduktion zugeführt werden können, wodurch eine vollständige stoffliche und energetische Nutzung der Silage erreicht wird.