TY - JOUR A1 - Martins, Berta M. A1 - Blaser, Martin A1 - Feliks, Mikolaj A1 - Ullmann, Matthias G. A1 - Buckel, Wolfgang A1 - Selmer, Thorsten T1 - Structural basis for a Kolbe-type decarboxylation catalyzed by a glycyl radical enzyme JF - Journal of the American Chemical Society Y1 - 2011 N1 - Just accepted manuscript SP - 1 EP - 33 PB - ACS Publications CY - Washington, DC ER - TY - GEN A1 - Martin, Conrad Steven A1 - Frauenrath, Tobias A1 - Zerdem, Celal A1 - Renz, Wolfgang A1 - Niendorf, Thoralf T1 - Evaluation of Magneto Alert Sensor (MALSE) to Improve MR Safety by Decreasing the Incidence of Ferromagnetic Projectile Accidents T2 - 2011 ISMRM Annual Meeting Proceedings N2 - The magnetic forces of fringe magnetic fields of MR systems on ferromagnetic components can impose a severe patient, occupational health and safety hazard. MRI accidents are listed as number 9 of the top 10 risks in modern medicine. With the advent of ultrahigh field MR systems including passively shielded magnet versions, this risk, commonly known as the missile or projectile effect is even more pronounced. A strategy employing magnetic field sensors which can be attached to ferromagnetic objects that are commonly used in a clinical environment is conceptually appealing for the pursuit of reducing the risk of ferromagnetic projectile accidents. Y1 - 2011 SN - 1545-4428 N1 - ISMRM 19th Annual Meeting & Exhibition, 7-13 May 2011, Montreal, Quebec, Canada ER - TY - JOUR A1 - Martin, Conrad A1 - Frauenrath, Tobias A1 - Özerdem, Celal A1 - Renz, Wolfgang A1 - Niendorf, Thoralf T1 - Development and evaluation of a small and mobile Magneto Alert Sensor (MALSE) to support safety requirements for magnetic resonance imaging JF - European Radiology N2 - Objective The purpose of this study is to (i) design a small and mobile Magnetic field ALert SEnsor (MALSE), (ii) to carefully evaluate its sensors to their consistency of activation/deactivation and sensitivity to magnetic fields, and (iii) to demonstrate the applicability of MALSE in 1.5 T, 3.0 T and 7.0 T MR fringe field environments. Methods MALSE comprises a set of reed sensors, which activate in response to their exposure to a magnetic field. The activation/deactivation of reed sensors was examined by moving them in/out of the fringe field generated by 7TMR. Results The consistency with which individual reed sensors would activate at the same field strength was found to be 100% for the setup used. All of the reed switches investigated required a substantial drop in ambient magnetic field strength before they deactivated. Conclusions MALSE is a simple concept for alerting MRI staff to a ferromagnetic object being brought into fringe magnetic fields which exceeds MALSEs activation magnetic field. MALSE can easily be attached to ferromagnetic objects within the vicinity of a scanner, thus creating a barrier for hazardous situations induced by ferromagnetic parts which should not enter the vicinity of an MR-system to occur. KW - MRI KW - MR safety KW - Magneto alert sensor KW - High field MRI KW - Uktrahigh field MRI Y1 - 2011 U6 - https://doi.org/10.1007/s00330-011-2153-z SN - 1432-1084 VL - 21 SP - 2187 EP - 2192 PB - Springer CY - Berlin, Heidelberg ER - TY - JOUR A1 - Manea, Marilena A1 - Leurs, Ulrike A1 - Orban, Erika A1 - Baranyai, Zsuzsa A1 - Öhlschläger, Peter A1 - Marquardt, Andreas A1 - Schulcz, Akos A1 - Tejeda, Miguel T1 - Enhanced Enzymatic Stability and Antitumor Activity of Daunorubicin-GnRH-III Bioconjugates Modified in Position 4 JF - Bioconjugate Chemistry Y1 - 2011 SN - 1520-4812 VL - 22 IS - 7 SP - 1320 EP - 1329 PB - ACS CY - Washington, DC ER - TY - JOUR A1 - Malzahn, Kerstin A1 - Windmiller, Joshua Ray A1 - Valdés-Ramírez, Gabriela A1 - Wang, Joseph A1 - Schöning, Michael Josef T1 - Wearable electrochemical sensors for in situ analysis in marine environments JF - Analyst. 136 (2011), H. 14 Y1 - 2011 SN - 0003-2654 SP - 2912 EP - 2917 PB - Royal Society of Chemistry CY - Cambridge ER - TY - JOUR A1 - Maier, M. M. A1 - Feucht, N. A1 - Winkler von Mohrenfels, C. A1 - Kotliar, Konstantin A1 - Fabian, E. A1 - Lohmann, C. P. T1 - Nahtlose Cerclage mit Skleratunnelfixation. Sutureless Encircling Band - Clinical Experience JF - Klinische Monatsblätter für Augenheilkunde Y1 - 2011 SN - 0344-6360 VL - 228 IS - 5 SP - 473 EP - 476 PB - Thieme CY - Stuttgart ER - TY - JOUR A1 - Lustfeld, H. A1 - Hirschfeld, J. A. A1 - Reißel, Martin A1 - Steffen, B. T1 - Enhancement of precision and reduction of measuring points in tomographic reconstructions JF - Physics Letters A Y1 - 2011 SN - 0375-9601 VL - 375 IS - 8 SP - 1167 EP - 1171 PB - Elsevier CY - Amsterdam ER - TY - CHAP A1 - Loeb, Horst W. A1 - Schartner, Karl-Heinz A1 - Dachwald, Bernd A1 - Ohndorf, Andreas A1 - Seboldt, Wolfgang T1 - An Interstellar – Heliopause mission using a combination of solar/radioisotope electric propulsion T2 - Presented at the 32nd International Electric Propulsion Conference N2 - There is common agreement within the scientific community that in order to understand our local galactic environment it will be necessary to send a spacecraft into the region beyond the solar wind termination shock. Considering distances of 200 AU for a new mission, one needs a spacecraft travelling at a speed of close to 10 AU/yr in order to keep the mission duration in the range of less than 25 yrs, a transfer time postulated by ESA.Two propulsion options for the mission have been proposed and discussed so far: the solar sail propulsion and the ballistic/radioisotope electric propulsion. As a further alternative, we here investigate a combination of solar-electric propulsion and radioisotope-electric propulsion. The solar-electric propulsion stage consists of six 22 cm diameter “RIT-22”ion thrusters working with a high specific impulse of 7377 s corresponding to a positive grid voltage of 5 kV. Solar power of 53 kW BOM is provided by a light-weight solar array. The REP-stage consists of four space-proven 10 cm diameter “RIT-10” ion thrusters that will be operating one after the other for 9 yrs in total. Four advanced radioisotope generators provide 648 W at BOM. The scientific instrument package is oriented at earlier studies. For its mass and electric power requirement 35 kg and 35 W are assessed, respectively. Optimized trajectory calculations, treated in a separate contribution, are based on our “InTrance” method.The program yields a burn out of the REP stage in a distance of 79.6 AU for a usage of 154 kg of Xe propellant. With a C3 = 45,1 (km/s)2 a heliocentric probe velocity of 10 AU/yr is reached at this distance, provided a close Jupiter gravity assist adds a velocity increment of 2.7 AU/yr. A transfer time of 23.8 yrs results for this scenario requiring about 450 kg Xe for the SEP stage, jettisoned at 3 AU. We interpret the SEP/REP propulsion as a competing alternative to solar sail and ballistic/REP propulsion. Omiting a Jupiter fly-by even allows more launch flexibility, leaving the mission duration in the range of the ESA specification. Y1 - 2011 N1 - 32nd International Electric Propulsion Conference, 11-15 September. Wiesbaden, Germany SP - 1 EP - 7 ER - TY - CHAP A1 - Lind, Thorsten Patric T1 - Wirkungen der Eröffnung des Insolvenzverfahrens : §§ 129, 132, 133, 144, 145 T2 - Bankenkommentar zum Insolvenzrecht Y1 - 2011 SN - 978-3-940976-55-0 SP - 1145 EP - 1585 PB - Finanz Colloquium CY - Heidelberg ER - TY - JOUR A1 - Lind, Thorsten Patric T1 - Handelndenhaftung bei Vorrats- oder Mantel-GmbH nur für vor Offenlegung der wirtschaftlichen Neugründung ohne Zustimmung aller Gesellschafter vorgenommene Geschäfte : BGH, Urteil vom 12.07.2011 - II ZR 71/11 : Anmerkung JF - Fachdienst Zivilrecht - LMK - Kommentierte BGH-Rechtsprechung, Lindenmaier-Möhring Y1 - 2011 SN - 1611-1095 IS - 11 PB - Beck CY - München ER -