TY  - JOUR
A1  - Lanzl, Ines M.
A1  - Seidova, Seid-Fatima
A1  - Maier, Mathias
A1  - Schmidt-Trucksäss, Arno
A1  - Halle, Martin
A1  - Kotliar, Konstantin
T1  - Dynamic retinal vessel response to flicker in age-related macular degeneration patients before and after vascular endothelial growth factor inhibitor injection
JF  - Acta Ophthalmologica
Y1  - 2011
SN  - 1755-3768
VL  - 89
IS  - 5
SP  - 472
EP  - 479
PB  - Wiley
CY  - Weinheim
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  - Mikielewicz, Marek
A1  - Kotliar, Konstantin
A1  - Barraquer, Rafael I.
A1  - Michael, Ralph
T1  - Air-pulse corneal applanation signal curve parameters for the characterisation of keratoconus
JF  - British Journal of Ophthalmology (eBJO)
Y1  - 2011
SN  - 1468-2079
VL  - 95
IS  - 6
SP  - 793
EP  - 798
PB  - BMJ Publ. Group
CY  - London
ER  - 
TY  - JOUR
A1  - Kotliar, Konstantin
A1  - Baumann, Marcus
A1  - Vilser, Walthard
A1  - Lanzl, Ines M.
T1  - Pulse wave velocity in retinal arteries of healthy volunteers
JF  - British Journal of Ophthalmology (eBJO)
Y1  - 2011
SN  - 1468-2079
VL  - 95
IS  - 11
SP  - 675
EP  - 679
PB  - BMJ Publ. Group
CY  - London
ER  - 
TY  - JOUR
A1  - Kotliar, Konstantin
A1  - Lanzl, Ines M.
A1  - Schmidt-Trucksäss, A.
A1  - Sitnikova, Diana
A1  - Ali, Mohammad
A1  - Blume, Katharina
A1  - Halle, Martin
A1  - Hansser, Henner
T1  - Dynamic retinal vessel response to flicker in obesity: A methodological approach
JF  - Microvascular Research
Y1  - 2011
SN  - 0026-2862
VL  - 81
IS  - 1
SP  - 123
EP  - 128
PB  - Elsevier
CY  - Amsterdam
ER  - 
TY  - JOUR
A1  - Dashevsky, Alexey V.
A1  - Lanzl, Ines M.
A1  - Kotliar, Konstantin
T1  - Non-penetrating intracanalicular partial trabeculectomy via the ostia of Schlemm's canal
JF  - Graefe's Archive for Clinical and Experimental Ophthalmology
Y1  - 2011
SN  - 0721-832x
VL  - 249
IS  - 4
SP  - 565
EP  - 573
PB  - Springer
CY  - Berlin
ER  - 
TY  - JOUR
A1  - Hanssen, H.
A1  - Nickel, T.
A1  - Drexel, V.
A1  - Hertel, G.
A1  - Emslander, I.
A1  - Sisic, Z.
A1  - Lorang, D.
A1  - Schuster, T.
A1  - Kotliar, Konstantin
A1  - Pressler, A.
A1  - Schmidt-Trucksäss, A.
A1  - Weis, M.
A1  - Halle, M.
T1  - Exercise-induced alterations of retinal vessel diameters and cardiovascular risk reduction in obesity
JF  - Atherosclerosis
Y1  - 2011
SN  - 0021-9150
VL  - 216
IS  - 2
SP  - 433
EP  - 439
PB  - Elsevier
CY  - Amsterdam
ER  - 
TY  - JOUR
A1  - Preiß, C.
A1  - Linder, Peter
A1  - Wendt, K.
A1  - Krystek, M.
A1  - Digel, Ilya
A1  - Gossmann, Matthias
A1  - Temiz Artmann, Aysegül
A1  - Porst, Dariusz
A1  - Kayser, Peter
A1  - Bassam, Rasha
A1  - Artmann, Gerhard
T1  - Engineering technology for plant physiology and plant stress research
N2  - Plant physiology and plant stress: Plant physiology will be much more important for human mankind because of yield and cultivation limits of crops determined by their resistance to stress. To assess and counteract various stress factors it is necessary to conduct plant research to gain information and results on plant physiology.
KW  - Pflanzenphysiologie
KW  - Pflanzenstress
KW  - Pflanzenscanner
KW  - plant stress
KW  - plant scanner
Y1  - 2011
ER  - 
TY  - JOUR
A1  - Doorschodt, B. M.
A1  - Schreinemachers, M. C. J. M.
A1  - Behbahani, Mehdi
A1  - Florquin, S.
A1  - Weis, J.
A1  - Staat, Manfred
A1  - Tolba, R. H.
T1  - Hypothermic machine perfusion of kidney grafts: which pressure is preferred
JF  - Annals of Biomedical Engineering. 39 (2011), H. 3
Y1  - 2011
SN  - 1573-9686
SP  - 1051
EP  - 1059
PB  - Springer
CY  - Berlin
ER  - 
TY  - CHAP
A1  - Ohndorf, Andreas
A1  - Dachwald, Bernd
A1  - Seboldt, Wolfgang
A1  - Schartner, Karl-Heinz
T1  - Flight times to the heliopause using a combination of solar and radioisotope electric propulsion
T2  - 32nd International Electric Propulsion Conference
N2  - We investigate the interplanetary flight of a low-thrust space probe to the heliopause,located at a distance of about 200 AU from the Sun. Our goal was to reach this distance within the 25 years postulated by ESA for such a mission (which is less ambitious than the 15-year goal set by NASA). Contrary to solar sail concepts and combinations of allistic and electrically propelled flight legs, we have investigated whether the set flight time limit could also be kept with a combination of solar-electric propulsion and a second, RTG-powered upper stage. The used ion engine type was the RIT-22 for the first stage and the RIT-10 for the second stage. Trajectory optimization was carried out with the low-thrust optimization program InTrance, which implements the method of Evolutionary Neurocontrol,using Artificial Neural Networks for spacecraft steering and Evolutionary Algorithms to optimize the Neural Networks’ parameter set. Based on a parameter space study, in which the number of thrust units, the unit’s specific impulse, and the relative size of the solar power generator were varied, we have chosen one configuration as reference. The transfer time of this reference configuration was 29.6 years and the fastest one, which is technically
more challenging, still required 28.3 years. As all flight times of this parameter study were longer than 25 years, we further shortened the transfer time by applying a launcher-provided hyperbolic excess energy up to 49 km2/s2. The resulting minimal flight time for the reference configuration was then 27.8 years. The following, more precise optimization to a launch with the European Ariane 5 ECA rocket reduced the transfer time to 27.5 years. This is the fastest mission design of our study that is flexible enough to allow a launch every
year. The inclusion of a fly-by at Jupiter finally resulted in a flight time of 23.8 years,which is below the set transfer-time limit. However, compared to the 27.5-year transfer,this mission design has a significantly reduced launch window and mission flexibility if the
escape direction is restricted to the heliosphere’s “nose".
KW  - low-thrust trajectory optimization
KW  - heliosphere
KW  - ion propulsion
Y1  - 2011
N1  - IEPC-2011-051
32nd International Electric Propulsion Conference,September 11–15, 2011
Wiesbaden, Germany
SP  - 1
EP  - 12
ER  -