TY  - CHAP
A1  - Schuh, G.
A1  - Gottschalk, S.
A1  - Höhne, Tim
A1  - Cloots, M.
ED  - Wenzel, Sigrid
T1  - Parametrierung einer Schlupfregelung in der simulativen Produktionsplanung
T2  - Simulation in Produktion und Logistik 2006 : Tagungsband zur 12. Fachtagung, Kassel, 26. - 27. September 2006
Y1  - 2006
SN  - 3-936150-48-6
N1  - ASIM-Mitteilung ; 104
SP  - 233
EP  - 243
ER  - 
TY  - JOUR
A1  - Schuh, G.
A1  - Kampker, A.
A1  - Höhne, Tim
T1  - Adaptive Logistik – Selbststeuerung in Fertigung und Montage
JF  - wt Werkstattstechnik online
Y1  - 2006
SN  - 1436-4980
VL  - 96
IS  - 5
SP  - 321
EP  - 324
ER  - 
TY  - JOUR
A1  - Bialonski, Stephan
A1  - Wellmer, Jörg
A1  - Elger, Christian E.
A1  - Lehnertz, Klaus
T1  - Interictal focus localization in neocortical lesional epilepsies with synchronization cluster analysis
JF  - Epilepsia
Y1  - 2006
SN  - 0013-9580
VL  - 47
SP  - 36
ER  - 
TY  - JOUR
A1  - Bialonski, Stephan
A1  - Lehnertz, Klaus
T1  - Identifying phase synchronization clusters in spatially extended dynamical systems
JF  - Physical Review E
Y1  - 2006
U6  - http://dx.doi.org/10.1103/PhysRevE.74.051909
SN  - 2470-0053
VL  - 74
IS  - 5
SP  - 051909
ER  - 
TY  - JOUR
A1  - Dethloff, Nina
A1  - Kroll-Ludwigs, Kathrin
T1  - The Constitutional Court as Driver of Reforms in German Family Law
JF  - International Survey of Family Law
Y1  - 2018
SP  - 217
EP  - 234
ER  - 
TY  - CHAP
A1  - Kroll-Ludwigs, Kathrin
ED  - Staake, Marco
T1  - Selbstverantwortung oder Vertrauenshaftung? – Anwendung von § 311 II Nr. 1 BGB (c.i.c.) auf Eheverträge und Angehörigenbürgschaften
T2  - Verantwortung und Haftung : Leipziger Tagung, 6. bis 9. September 2006 ; Jahrbuch Junger Zivilrechtswissenschaftler 2006 ; [17. Tagung der Gesellschaft Junger Zivilrechtswissenschaftler e.V.]
Y1  - 2006
SP  - 118
EP  - 145
ER  - 
TY  - CHAP
A1  - Drumm, Christian
A1  - Lemcke, Jens
A1  - Oberle, Daniel
T1  - Integrating Semantic Web Services and Business Process Management: A Real Use Case
T2  - Proceedings of the ESWC 2006 Workshop Semantics for Business Process Management 2006 (SBPM 2006), June 2006
Y1  - 2006
ER  - 
TY  - JOUR
A1  - Stanley, Lesley A.
A1  - Horsburgh, Brian C.
A1  - Ross, Jillian
A1  - Scheer, Nico
A1  - Wolf, C. Roland
T1  - Nuclear Receptors which play a pivotal role in drug disposition and chemical toxicity
JF  - Drug Metabolism Reviews
Y1  - 2006
U6  - http://dx.doi.org/10.1080/03602530600786232
SN  - 1097-9883
VL  - 38
IS  - 3
SP  - 515
EP  - 597
ER  - 
TY  - JOUR
A1  - Reugels, Alexander M.
A1  - Boggetti, Barbara
A1  - Scheer, Nico
A1  - Campos-Ortega, José A.
T1  - Asymmetric localization of Numb:EGFP in dividing neuroepithelial cells during neurulation in Danio rerio
JF  - Developmental Dynamics
Y1  - 2006
U6  - http://dx.doi.org/10.1002/dvdy.20699
SN  - 1097-0177
VL  - 235
IS  - 4
SP  - 934
EP  - 948
ER  - 
TY  - CHAP
A1  - Loeb, Horst W.
A1  - Schartner, Karl-Heinz
A1  - Seboldt, Wolfgang
A1  - Dachwald, Bernd
A1  - Streppel, Joern
A1  - Meusemann, Hans
A1  - Schülke, Peter
T1  - SEP for a lander mission to the jovian moon europa
T2  - 57th International Astronautical Congress
N2  - Under DLR-contract, Giessen University and DLR Cologne are studying solar-electric propulsion missions (SEP) to the outer regions of the solar system. The most challenging reference mission concerns the transport of a 1.35-tons chemical lander spacecraft into an 80-RJ circular orbit around Jupiter, which would enable to place a 375 kg lander with 50 kg of scientific instruments on the surface of the icy moon "Europa". Thorough analyses show that the best solution in terms of SEP launch mass times thrusting time would be a two-stage EP module and a triple-junction solar array with concentrators which would be deployed step by step. Mission performance optimizations suggest to propel the spacecraft in the first EP stage by 6 gridded ion thrusters, running at 4.0 kV of beam voltage, which would save launch mass, and in the second stage by 4 thrusters with 1.25 to 1.5 kV of positive high voltage saving thrusting time. In this way, the launch mass of the spacecraft would be kept within 5.3 tons. Without a launcher's C3 and interplanetary gravity assists, Jupiter might be reached within about 4 yrs. The spiraling-down into the parking orbit would need another 1.8 yrs. This "large mission" can be scaled down to a smaller one, e.g., by halving all masses, the solar array power, and the number of thrusters. Due to their reliability, long lifetime and easy control, RIT-22 engines have been chosen for mission analysis. Based on precise tests, the thruster performance has been modeled.
Y1  - 2006
U6  - http://dx.doi.org/10.2514/6.IAC-06-C4.4.04
N1  - 57th International Astronautical Congress, 02 October 2006 - 06 October 2006, Valencia, Spain.
SP  - 1
EP  - 12
ER  -