Seefeldt, Patric und Spröwitz, Tom und Grundmann, Jan Thimo (2016) Verification Testing of the Gossamer-1 Deployment Demonstrator. In: Proceedings of the 67th International Astronautical Congress. 67th Internationa Astronautical Congress (IAC), 2016-09-26 - 2016-09-30, Guadalajara, Mexico. ISBN 9781510835825.
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Kurzfassung
Gossamer structures for innovative space applications, such as solar sails, require a technology that allows their controlled and thereby safe deployment. Before employing such technology for a dedicated science mission, it is necessary, to demonstrate its reliability with a Technology Readiness Level of six or higher. The aim of the presented work is to provide a reliable technology that enables the controlled deployment and verification of its functionality with various laboratory tests to qualify the hardware for a first demonstration in low Earth orbit. The development was made in the Gossamer-1 project of the German Aerospace Center. This presentation provides an overview of the Gossamer-1 hardware development. The design is based on a crossed boom configuration with triangular sail segments. Employing engineering models, all aspects of the deployment were tested under ambient environment. Several components were also subjected to environmental qualification testing. An innovative stowing and deployment strategy for a controlled deployment and the required mechanisms are described. The tests conducted provide insight into the deployment process and allow a mechanical characterization of this process, in particular the measurement of the deployment forces. Deployment on system level could partially be demonstrated to be robust and controllable. The deployment technology is on Technology Readiness Level four approaching level five, with a qualification model for environmental testing currently being built.
elib-URL des Eintrags: | https://elib.dlr.de/106399/ | ||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||
Titel: | Verification Testing of the Gossamer-1 Deployment Demonstrator | ||||||||||||||||
Autoren: |
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Datum: | 2016 | ||||||||||||||||
Erschienen in: | Proceedings of the 67th International Astronautical Congress | ||||||||||||||||
Referierte Publikation: | Nein | ||||||||||||||||
Open Access: | Ja | ||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||
ISBN: | 9781510835825 | ||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||
Stichwörter: | deployment systems, deployable structures, deployable membranes, verification testing, mechanisms, solar sailing | ||||||||||||||||
Veranstaltungstitel: | 67th Internationa Astronautical Congress (IAC) | ||||||||||||||||
Veranstaltungsort: | Guadalajara, Mexico | ||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||
Veranstaltungsbeginn: | 26 September 2016 | ||||||||||||||||
Veranstaltungsende: | 30 September 2016 | ||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||
HGF - Programm: | Raumfahrt | ||||||||||||||||
HGF - Programmthema: | Technik für Raumfahrtsysteme | ||||||||||||||||
DLR - Schwerpunkt: | Raumfahrt | ||||||||||||||||
DLR - Forschungsgebiet: | R SY - Technik für Raumfahrtsysteme | ||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | R - Entfaltungstechnologie . Solar Sail (alt) | ||||||||||||||||
Standort: | Bremen | ||||||||||||||||
Institute & Einrichtungen: | Institut für Raumfahrtsysteme > Mechanik und Thermalsysteme | ||||||||||||||||
Hinterlegt von: | Sznajder, Dr.-Ing. Maciej | ||||||||||||||||
Hinterlegt am: | 05 Okt 2016 15:09 | ||||||||||||||||
Letzte Änderung: | 24 Apr 2024 20:11 |
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