TY - JOUR A1 - Seibler, Jost A1 - Zevnik, Branko A1 - Küter-Luks, Birgit A1 - Andreas, Susanne A1 - Kern, Heidrun A1 - Hennek, Thomas A1 - Rode, Anja A1 - Heimann, Cornelia A1 - Faust, Nicole A1 - Kauselmann, Gunther A1 - Schoor, Michael A1 - Jaenisch, Rudolf A1 - Rajewsky, Klaus A1 - Kühn, Ralf A1 - Schwenk, Frieder T1 - Rapid generation of inducible mouse mutants JF - Nucleic Acids Research Y1 - 2003 U6 - http://dx.doi.org/10.1093/nar/gng012 SN - 1362-4962 VL - 33 IS - 4 SP - e12 ER - TY - JOUR A1 - Seibler, Jost A1 - Schübeler, Dirk A1 - Fiering, Steven A1 - Groudine, Mark A1 - Bode, Jürgen T1 - DNA cassette exchange in ES cells mediated by Flp recombinase: an efficient strategy for repeated modification of tagged loci by marker-free constructs JF - Biochemistry Y1 - 1998 U6 - http://dx.doi.org/10.1021/bi980288t SN - 1520-4995 VL - 37 IS - 18 SP - 6229 EP - 6234 ER - TY - CHAP A1 - Seibler, Jost A1 - Schwenk, Frieder T1 - Transgenic RNAi Applications in the Mouse T2 - Methods in Enzymology : Guide to Techniques in Mouse Development, Part B: Mouse Molecular Genetics. 2nd Edition Y1 - 2010 SN - 978-0-12-384880-2 N1 - Methods in Enzymology : Vol. 477 SP - 367 EP - 386 PB - Elsevier CY - Amsterdam ER - TY - JOUR A1 - Seibler, Jost A1 - Küter-Luks, Birgit A1 - Kern, Heidrun A1 - Streu, Sandra A1 - Plum, Leona A1 - Maurer, Jan A1 - Kühn, Ralf A1 - Brüning, Jens C. A1 - Schwenk, Frieder T1 - Single copy shRNA configuration for ubiquitous gene knockdown in mice JF - Nucleic Acids Research Y1 - 2005 U6 - http://dx.doi.org/10.1093/nar/gni065 SN - 1362-4962 VL - 33 IS - 7 SP - e67 ER - TY - JOUR A1 - Seibler, Jost A1 - Kleinridders, Andre A1 - Küter-Luks, Birgit A1 - Niehaves, Sandra A1 - Brüning, Jens C. A1 - Schwenk, Frieder T1 - Reversible gene knockdown in mice using a tight, inducible shRNA expression system JF - Nucleic Acids Research Y1 - 2007 U6 - http://dx.doi.org/10.1093/nar/gkm122 SN - 1362-4962 VL - 35 IS - 7 SP - e54 ER - TY - JOUR A1 - Seibler, Jost A1 - Bode, Jürgen T1 - Double-reciprocal crossover mediated by FLP-recombinase: a concept and an assay JF - Biochemistry Y1 - 1997 SN - 1520-4995 VL - 36 IS - 7 SP - 1740 EP - 1747 ER - TY - JOUR A1 - Seefeldt, Patric A1 - Dachwald, Bernd T1 - Temperature increase on folded solar sail membranes JF - Advances in Space Research Y1 - 2021 U6 - http://dx.doi.org/10.1016/j.asr.2020.09.026 SN - 0273-1177 VL - 67 IS - 9 SP - 2688 EP - 2695 PB - Elsevier CY - Amsterdam ER - TY - CHAP A1 - Seefeldt, Patric A1 - Bauer, Waldemar A1 - Dachwald, Bernd A1 - Grundmann, Jan Thimo A1 - Straubel, Marco A1 - Sznajder, Maciej A1 - Tóth, Norbert A1 - Zander, Martin E. T1 - Large lightweight deployable structures for planetary defence: solar sail propulsion, solar concentrator payloads, large-scale photovoltaic power T2 - 4th IAA Planetary Defense Conference - PDC 2015, 13-17 April 2015, Frascati, Roma, Italy Y1 - 2015 N1 - IAA-PDC-15-P-20 ER - TY - CHAP A1 - Sedlacek, G. A1 - Geßler, A. A1 - Schleser, Markus A1 - Mund, F. A1 - Völling, B. T1 - Verbindungen vorgefertigter Textilbetonbauteile T2 - Textile reinforced structures : proceedings of the 2nd Colloquium on Textile Reinforced Structures (CTRS2), Dresden, Germany, 29.9. - 1.10.2003 Y1 - 2003 SN - 3-86005-386-8 SP - 481 EP - 493 PB - Techn. Univ. CY - Dresden ER - TY - CHAP A1 - Seboldt, Wolfgang A1 - Dachwald, Bernd T1 - Solar sails for near-term advanced scientific deep space missions T2 - Proceedings of the 8th International Workshop on Combustion and Propulsion N2 - 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. KW - solar sail KW - low-thrust KW - near-Earth asteroid KW - sample return KW - solar system Y1 - 2003 N1 - Proceedings of the 8th International Workshop on Combustion and Propulsion. Pozzuoli, Italy, 16 - 21 June 2002. ER -