TY - JOUR A1 - Gömmel, Andreas A1 - Butenweg, Christoph A1 - Bolender, Katrin A1 - Grunendahl, Arno T1 - A muscle controlled finite-element model of laryngeal abduction and adduction JF - Computer methods in biomechanics and biomedical engineering Y1 - 2007 SN - 1476-8259 (E-Journal); 1025-5842 (Print) VL - Volume 10 IS - Issue 5 SP - 377 EP - 388 ER - TY - JOUR A1 - Butenweg, Christoph A1 - Gellert, Christoph A1 - Meskouris, Konstantin T1 - Mauerwerkswände unter zyklischer Schubbeanspruchung JF - Mauerwerk : European journal of masonry Y1 - 2007 U6 - https://doi.org/10.1002/dama.200700356 SN - 1437-1022 (E-Journal); 1432-3427 (Print) VL - Volume 11 IS - Issue 6 SP - 356 EP - 362 ER - TY - BOOK A1 - Meskouris, Konstantin A1 - Renault, Philippe A1 - Butenweg, Christoph A1 - Hinzen, Klaus-G. A1 - Weber, Bernd T1 - Gefährdungsabschätzung von Brücken in Deutschland unter Erdbebenbelastung. [Bericht zum Forschungs- und Entwicklungsvorhaben FE 15.393/2003/FRB des Bundesministeriums für Verkehr, Bau und Stadtentwicklung.] (Forschung Straßenbau und Straßenverkehrstechnik ; 952) Y1 - 2007 SN - 978-3-86509-602-9 PB - Bundesministerium für Verkehr, Bau und Stadtentwicklung, Abt. Straßenbau, Straßenverkehr CY - Bonn ER - TY - CHAP A1 - Meskouris, Konstantin A1 - Butenweg, Christoph A1 - Kalker, Ines A1 - Mistler, Michael T1 - Numerical simulation of historic masonry buildings T2 - Antike Erdbeben im alpinen und zirkumalpinen Raum : Befunde und Probleme in archäologischer, historischer und seismologischer Sicht ; Beiträge des Interdisziplinären Workshops Schloss Hohenkammer, 14./15. Mai 2004 = Earthquakes in antiquity in the alpine and circum-alpine region / Gerhard H. Waldherr ; Anselm Smolka (Hrsg.) (Geographica Historica ; 24) Y1 - 2007 SN - 978-3-515-09030-8 ; 3-515-09030-4 SP - 171 EP - 189 PB - Franz Steiner Verlag CY - Stuttgart ER - TY - CHAP A1 - Butenweg, Christoph A1 - Gellert, Christoph T1 - Berechnung und Bemessung von durch Erdbeben beanspruchten Mauerwerksbauten nach DIN 4149 (04.2005) T2 - Mauerwerksbau-Praxis / Schubert ; Schneider ; Schoch (Hrsg.) Y1 - 2007 SN - 3-9343-6938-3 ; 978-3-9343-6938-2 SP - 363 EP - 393 PB - Werner Verlag CY - Berlin ER - TY - BOOK A1 - Meskouris, Konstantin A1 - Hinzen, Klaus-Günter A1 - Butenweg, Christoph A1 - Mistler, Michael T1 - Bauwerke und Erdbeben : Grundlagen - Anwendung - Beispiele Y1 - 2007 SN - 3-8348-0146-1 ; 978-3-8348-0146-3 N1 - gedruckt in der Bereichsbibliothek Bayernallee unter der Signatur 11 XBM 41(2) vorhanden PB - Vieweg CY - Wiesbaden ET - 2., erweiterte und aktualisierte Auflage ER - TY - JOUR A1 - Zerlin, Kay A1 - Digel, Ilya A1 - Stadler, Andreas M. A1 - Büldt, Georg A1 - Zaccai, Guiseppe A1 - Artmann, Gerhard T1 - Dynamics and interactions of hemoglobin in human red blood cells and concentrated hemoglobin solutions JF - Regenerative medicine. 2 (2007), H. 5 Y1 - 2007 SN - 1746-0751 N1 - Proceedings of the 3rd World Congress on Regenerative Medicine. October 18-20, 2007. Leipzig, Germany SP - 573 EP - 573 ER - TY - JOUR A1 - Artmann, Gerhard A1 - Zerlin, Kay A1 - Digel, Ilya A1 - Stadler, Andreas M. T1 - Physical discontinuities at body temperature in human red blood cells / Artmann, GM ; Zerlin, K ; Digel, I ; Stadler, A ; Zaccai, G ; Temiz, AA JF - Tissue Engineering. 13 (2007), H. 7 Y1 - 2007 SN - 1076-3279 N1 - TERMIS-EU Meeting Abstracts London, UK September 4–7, 2007 SP - 1778 EP - 1778 ER - TY - CHAP A1 - Dachwald, Bernd A1 - Seboldt, Wolfgang A1 - Loeb, Horst W. A1 - Schartner, Karl-Heinz T1 - A comparison of SEP and NEP for a main belt asteroid sample return mission T2 - 7th International Symposium on Launcher Technologies, Barcelona, Spain, 02-05 April 2007 N2 - Innovative interplanetary deep space missions, like a main belt asteroid sample return mission, require ever larger velocity increments (∆V s) and thus ever more demanding propulsion capabilities. Providing much larger exhaust velocities than chemical high-thrust systems, electric low-thrust space-propulsion systems can significantly enhance or even enable such high-energy missions. In 1995, a European-Russian Joint Study Group (JSG) presented a study report on “Advanced Interplanetary Missions Using Nuclear-Electric Propulsion” (NEP). One of the investigated reference missions was a sample return (SR) from the main belt asteroid (19) Fortuna. The envisaged nuclear power plant, Topaz-25, however, could not be realized and also the worldwide developments in space reactor hardware stalled. In this paper, we investigate, whether such a mission is also feasible using a solar electric propulsion (SEP) system and compare our SEP results to corresponding NEP results. Y1 - 2007 SP - 1 EP - 10 ER - TY - CHAP A1 - Dachwald, Bernd A1 - Kahle, Ralph A1 - Wie, Bong T1 - Head-on impact deflection of NEAs: a case study for 99942 Apophis T2 - Planetary Defense Conference 2007 N2 - Near-Earth asteroid (NEA) 99942 Apophis provides a typical example for the evolution of asteroid orbits that lead to Earth-impacts after a close Earth-encounter that results in a resonant return. Apophis will have a close Earth-encounter in 2029 with potential very close subsequent Earth-encounters (or even an impact) in 2036 or later, depending on whether it passes through one of several less than 1 km-sized gravitational keyholes during its 2029-encounter. A pre-2029 kinetic impact is a very favorable option to nudge the asteroid out of a keyhole. The highest impact velocity and thus deflection can be achieved from a trajectory that is retrograde to Apophis orbit. With a chemical or electric propulsion system, however, many gravity assists and thus a long time is required to achieve this. We show in this paper that the solar sail might be the better propulsion system for such a mission: a solar sail Kinetic Energy Impactor (KEI) spacecraft could impact Apophis from a retrograde trajectory with a very high relative velocity (75-80 km/s) during one of its perihelion passages. The spacecraft consists of a 160 m × 160 m, 168 kg solar sail assembly and a 150 kg impactor. Although conventional spacecraft can also achieve the required minimum deflection of 1 km for this approx. 320 m-sized object from a prograde trajectory, our solar sail KEI concept also allows the deflection of larger objects. For a launch in 2020, we also show that, even after Apophis has flown through one of the gravitational keyholes in 2029, the solar sail KEI concept is still feasible to prevent Apophis from impacting the Earth, but many KEIs would be required for consecutive impacts to increase the total Earth-miss distance to a safe value Y1 - 2007 N1 - Planetary Defense Conference 2007, Wahington D.C., USA, 05-08 March 2007 SP - 1 EP - 12 ER -