@article{SeiblerZevnikKueterLuksetal.2003, author = {Seibler, Jost and Zevnik, Branko and K{\"u}ter-Luks, Birgit and Andreas, Susanne and Kern, Heidrun and Hennek, Thomas and Rode, Anja and Heimann, Cornelia and Faust, Nicole and Kauselmann, Gunther and Schoor, Michael and Jaenisch, Rudolf and Rajewsky, Klaus and K{\"u}hn, Ralf and Schwenk, Frieder}, title = {Rapid generation of inducible mouse mutants}, series = {Nucleic Acids Research}, volume = {33}, journal = {Nucleic Acids Research}, number = {4}, issn = {1362-4962}, doi = {10.1093/nar/gng012}, pages = {e12}, year = {2003}, language = {en} } @article{SeiblerSchuebelerFieringetal.1998, author = {Seibler, Jost and Sch{\"u}beler, Dirk and Fiering, Steven and Groudine, Mark and Bode, J{\"u}rgen}, title = {DNA cassette exchange in ES cells mediated by Flp recombinase: an efficient strategy for repeated modification of tagged loci by marker-free constructs}, series = {Biochemistry}, volume = {37}, journal = {Biochemistry}, number = {18}, issn = {1520-4995}, doi = {10.1021/bi980288t}, pages = {6229 -- 6234}, year = {1998}, language = {en} } @incollection{SeiblerSchwenk2010, author = {Seibler, Jost and Schwenk, Frieder}, title = {Transgenic RNAi Applications in the Mouse}, series = {Methods in Enzymology : Guide to Techniques in Mouse Development, Part B: Mouse Molecular Genetics. 2nd Edition}, booktitle = {Methods in Enzymology : Guide to Techniques in Mouse Development, Part B: Mouse Molecular Genetics. 2nd Edition}, publisher = {Elsevier}, address = {Amsterdam}, isbn = {978-0-12-384880-2}, pages = {367 -- 386}, year = {2010}, language = {en} } @article{SeiblerKueterLuksKernetal.2005, author = {Seibler, Jost and K{\"u}ter-Luks, Birgit and Kern, Heidrun and Streu, Sandra and Plum, Leona and Maurer, Jan and K{\"u}hn, Ralf and Br{\"u}ning, Jens C. and Schwenk, Frieder}, title = {Single copy shRNA configuration for ubiquitous gene knockdown in mice}, series = {Nucleic Acids Research}, volume = {33}, journal = {Nucleic Acids Research}, number = {7}, issn = {1362-4962}, doi = {10.1093/nar/gni065}, pages = {e67}, year = {2005}, language = {en} } @article{SeiblerKleinriddersKueterLuksetal.2007, author = {Seibler, Jost and Kleinridders, Andre and K{\"u}ter-Luks, Birgit and Niehaves, Sandra and Br{\"u}ning, Jens C. and Schwenk, Frieder}, title = {Reversible gene knockdown in mice using a tight, inducible shRNA expression system}, series = {Nucleic Acids Research}, volume = {35}, journal = {Nucleic Acids Research}, number = {7}, issn = {1362-4962}, doi = {10.1093/nar/gkm122}, pages = {e54}, year = {2007}, language = {en} } @article{SeiblerBode1997, author = {Seibler, Jost and Bode, J{\"u}rgen}, title = {Double-reciprocal crossover mediated by FLP-recombinase: a concept and an assay}, series = {Biochemistry}, volume = {36}, journal = {Biochemistry}, number = {7}, issn = {1520-4995}, pages = {1740 -- 1747}, year = {1997}, language = {en} } @article{SeefeldtDachwald2021, author = {Seefeldt, Patric and Dachwald, Bernd}, title = {Temperature increase on folded solar sail membranes}, series = {Advances in Space Research}, volume = {67}, journal = {Advances in Space Research}, number = {9}, publisher = {Elsevier}, address = {Amsterdam}, issn = {0273-1177}, doi = {10.1016/j.asr.2020.09.026}, pages = {2688 -- 2695}, year = {2021}, language = {en} } @inproceedings{SeefeldtBauerDachwaldetal.2015, author = {Seefeldt, Patric and Bauer, Waldemar and Dachwald, Bernd and Grundmann, Jan Thimo and Straubel, Marco and Sznajder, Maciej and T{\´o}th, Norbert and Zander, Martin E.}, title = {Large lightweight deployable structures for planetary defence: solar sail propulsion, solar concentrator payloads, large-scale photovoltaic power}, series = {4th IAA Planetary Defense Conference - PDC 2015, 13-17 April 2015, Frascati, Roma, Italy}, booktitle = {4th IAA Planetary Defense Conference - PDC 2015, 13-17 April 2015, Frascati, Roma, Italy}, pages = {24}, year = {2015}, language = {en} } @inproceedings{SedlacekGesslerSchleseretal.2003, author = {Sedlacek, G. and Geßler, A. and Schleser, Markus and Mund, F. and V{\"o}lling, B.}, title = {Verbindungen vorgefertigter Textilbetonbauteile}, series = {Textile reinforced structures : proceedings of the 2nd Colloquium on Textile Reinforced Structures (CTRS2), Dresden, Germany, 29.9. - 1.10.2003}, booktitle = {Textile reinforced structures : proceedings of the 2nd Colloquium on Textile Reinforced Structures (CTRS2), Dresden, Germany, 29.9. - 1.10.2003}, publisher = {Techn. Univ.}, address = {Dresden}, organization = {Colloquium on Textile Reinforced Structures <2, 2003, Dresden>}, isbn = {3-86005-386-8}, pages = {481 -- 493}, year = {2003}, language = {en} } @inproceedings{SeboldtDachwald2003, author = {Seboldt, Wolfgang and Dachwald, Bernd}, title = {Solar sails for near-term advanced scientific deep space missions}, series = {Proceedings of the 8th International Workshop on Combustion and Propulsion}, booktitle = {Proceedings of the 8th International Workshop on Combustion and Propulsion}, pages = {14 Seiten}, year = {2003}, abstract = {Solar sails are propelled in space by reflecting solar photons off large mirroring surfaces, thereby transforming the momentum of the photons into a propulsive force. This innovative concept for low-thrust space propulsion works without any propellant and thus provides a wide range of opportunities for highenergy low-cost missions. Offering an efficient way of propulsion, solar sailcraft could close a gap in transportation options for highly demanding exploration missions within our solar system and even beyond. On December 17th, 1999, a significant step was made towards the realization of this technology: a lightweight solar sail structure with an area of 20 m × 20 m was successfully deployed on ground in a large facility at the German Aerospace Center (DLR) at Cologne. The deployment from a package of 60 cm × 60 cm × 65 cm with a total mass of less than 35 kg was achieved using four extremely light-weight carbon fiber reinforced plastics (CFRP) booms with a specific mass of 100 g/m. The paper briefly reviews the basic principles of solar sails as well as the technical concept and its realization in the ground demonstration experiment, performed in close cooperation between DLR and ESA. Next possible steps are outlined. They could comprise the in-orbit demonstration of the sail deployment on the upper stage of a low-cost rocket and the verification of the propulsion concept by an autonomous and free flying solar sail in the frame of a scientific mission. It is expected that the present design could be extended to sail sizes of about (40 m)2 up to even (70 m)2 without significant mass penalty. With these areas, the maximum achievable thrust at 1 AU would range between 10 and 40 mN - comparable to some electric thrusters. Such prototype sails with a mass between 50 and 150 kg plus a micro-spacecraft of 50 to 250 kg would have a maximum acceleration in the order of 0.1 mm/s2 at 1 AU, corresponding to a maximum ∆V-capability of about 3 km/s per year. Two near/medium-term mission examples to a near-Earth asteroid (NEA) will be discussed: a rendezvous mission and a sample return mission.}, language = {en} }