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Hillebrandt, Martin und Meyer, Sebastian und Zander, Martin und Straubel, Marco und Hühne, Christian (2014) The Boom Design of the De-Orbit Sail Satellite. In: European Conference on Spacecraft Structures, Materials and Mechanical Testing. EUROPEAN CONFERENCE on SPACECRAFT STRUCTURES, MATERIALS & Environmental Testing, 01.-04.04.2014, Braunschweig, Germany.
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Kurzfassung
DE-ORBIT SAIL is a cubesat based drag sail for the de-orbiting of satellites in a low earth orbit. It is scheduled for launch in late 2014 and will deploy a 25m² sail supported by deployable carbon fiber booms designed and manufactured by DLR. This boom possesses a closed cross-section formed by two omega-shaped half-shells. Due to this cross-sectional design the boom features a high torsional stiffness. Thereby a high bending strength is achieved compared to other boom concepts for similar applications as the boom is less sensitive to flexural torsional buckling. The boom concept selection is based on a detailed analysis of three types of deployable booms which differ in their cross-sectional design. From this analysis the double-omega boom was determined as most suited for DE-ORBIT SAIL. For the manufacturing of the booms a novel method is used where the booms are manufactured in an integral way in one piece.
| elib-URL des Eintrags: | https://elib.dlr.de/95684/ | ||||||||||||||||||||||||
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| Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||||||
| Titel: | The Boom Design of the De-Orbit Sail Satellite | ||||||||||||||||||||||||
| Autoren: |
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| Datum: | April 2014 | ||||||||||||||||||||||||
| Erschienen in: | European Conference on Spacecraft Structures, Materials and Mechanical Testing | ||||||||||||||||||||||||
| Referierte Publikation: | Ja | ||||||||||||||||||||||||
| Open Access: | Ja | ||||||||||||||||||||||||
| Gold Open Access: | Nein | ||||||||||||||||||||||||
| In SCOPUS: | Nein | ||||||||||||||||||||||||
| In ISI Web of Science: | Ja | ||||||||||||||||||||||||
| Status: | veröffentlicht | ||||||||||||||||||||||||
| Stichwörter: | Deployable strcuture, boom, drag augmentation, solar sail | ||||||||||||||||||||||||
| Veranstaltungstitel: | EUROPEAN CONFERENCE on SPACECRAFT STRUCTURES, MATERIALS & Environmental Testing | ||||||||||||||||||||||||
| Veranstaltungsort: | Braunschweig, Germany | ||||||||||||||||||||||||
| Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||||||
| Veranstaltungsdatum: | 01.-04.04.2014 | ||||||||||||||||||||||||
| Veranstalter : | DLR, ESA, CNES | ||||||||||||||||||||||||
| 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: | Braunschweig | ||||||||||||||||||||||||
| Institute & Einrichtungen: | Institut für Faserverbundleichtbau und Adaptronik > Funktionsleichtbau | ||||||||||||||||||||||||
| Hinterlegt von: | Hillebrandt, Martin | ||||||||||||||||||||||||
| Hinterlegt am: | 31 Mär 2015 13:56 | ||||||||||||||||||||||||
| Letzte Änderung: | 20 Jun 2021 15:46 |
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