Dokument-ID Dokumenttyp Verfasser/Autoren Herausgeber Haupttitel Abstract Auflage Verlagsort Verlag Erscheinungsjahr Seitenzahl Schriftenreihe Titel Schriftenreihe Bandzahl ISBN Quelle der Hochschulschrift Konferenzname Bemerkung Quelle:Titel Quelle:Jahrgang Quelle:Heftnummer Quelle:Erste Seite Quelle:Letzte Seite URN DOI Zugriffsart Link Abteilungen OPUS4-8287 Konferenzveröffentlichung Grundmann, Jan Thimo, ; Meß, Jan-Gerd, ; Biele, Jens, ; Seefeldt, Patric, ; Dachwald, Bernd, dachwald@fh-aachen.de; Spietz, Peter, ; Grimm, Christian D., ; Spröwitz, Tom, ; Lange, Caroline, ; Ulamec, Stephan, Small spacecraft in small solar system body applications 2017 19 IEEE Aerospace Conference 2017, Big Sky, Montana, USA 978-1-5090-1613-6 Article No 7943626 1 20 10.1109/AERO.2017.7943626 campus https://doi.org/10.1109/AERO.2017.7943626 Fachbereich Luft- und Raumfahrttechnik OPUS4-10016 Konferenzveröffentlichung Grundmann, Jan Thimo, ; Biele, Jens, ; Dachwald, Bernd, Dachwald@fh-aachen.de; Grimm, Christian D., ; Lange, Caroline, ; Ulamec, Stephan, ; Ziach, Christian, ; Spröwitz, Tom, ; Ruffer, Michael, ; Seefeldt, Patric, ; Spietz, Peter, ; Toth, Norbert, ; Mimasu, Yuya, ; Rittweger, Andreas, ; Bibring, Jean-Pierre, ; Braukhane, Andy, ; Boden, Ralf Christian, ; Dumont, Etienne, ; Jahnke, Stephan Siegfried, ; Jetzschmann, Michael, ; Krüger, Hans, ; Lange, Michael, ; Gomez, Antonio Martelo, ; Massonett, Didier, ; Okada, Tatsuaki, ; Sagliano, Marco, ; Sasaki, Kaname, ; Schröder, Silvio, ; Sippel, Martin, ; Skoczylas, Thomas, ; Wejmo, Elisabet, Small landers and separable sub-spacecraft for near-term solar sails Following the successful PHILAE landing with ESA's ROSETTA probe and the launch of the MINERVA rovers and the Mobile Asteroid Surface Scout, MASCOT, aboard the JAXA space probe, HAYABUSA2, to asteroid (162173) Ryugu, small landers have found increasing interest. Integrated at the instrument level in their mothership they support small solar system body studies. With efficient capabilities, resource-friendly design and inherent robustness they are an attractive exploration mission element. We discuss advantages and constraints of small sub-spacecraft, focusing on emerging areas of activity such as asteroid diversity studies, planetary defence, and asteroid mining, on the background of our projects PHILAE, MASCOT, MASCOT2, the JAXA-DLR Solar Power Sail Lander Design Study, and others. The GOSSAMER-1 solar sail deployment concept also involves independent separable sub-spacecraft operating synchronized to deploy the sail. Small spacecraft require big changes in the way we do things and occasionally a little more effort than would be anticipated based on a traditional large spacecraft approach. In a Constraints-Driven Engineering environment we apply Concurrent Design and Engineering (CD/CE), Concurrent Assembly, Integration and Verification (CAIV) and Model-Based Systems Engineering (MBSE). Near-term solar sails will likely be small spacecraft which we expect to harmonize well with nano-scale separable instrument payload packages. 2017 10 The Fourth International Symposium on Solar Sailing 2017 The Fourth International Symposium on Solar Sailing 2017, 17-20 January 2017. Kyoto Research Park, Kyoto, Japan 1 10 weltweit https://elib.dlr.de/118803/1/17094_Paper_Mr.%20Jan%20Thimo%20Grundmann.pdf Fachbereich Luft- und Raumfahrttechnik