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Environmental Testing and Analysis of a Boom Deployment Mechanism for Gossamer-2

Meyer, Sebastian and Zander, Martin and Straubel, Marco and Hühne, Christian (2015) Environmental Testing and Analysis of a Boom Deployment Mechanism for Gossamer-2. 66th International Astronautical Congress, 12.-16. Okt. 2015, Jerusalem, Israel. (Unpublished)

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Abstract

DLR is currently developing several mechanisms for boom and membrane deploying spacecrafts. Two of the related projects are dedicated to solar sailing technology to investigate this promising alternative space propulsion technology. One supports the Gossamer-1 mission in which a 5 m by 5 m solar sail technology demonstrator is developed; the second is the planned, up scaled successor Gossamer-2 with a size of 20 m x 20 m. One goal of the development process in these missions is to achieve a deployment mechanism, that can be scaled up and used in future missions with larger sail areas (Gossamer-2: 20 m x 20 m, Gossamer-3: 50 m x 50 m) spanned out by larger booms. Within the EU funded DEPLOYTECH project the well matured Gossamer-1 boom deployment mechanism has been adapted for the Gossamer-2 size. Therefore, DLR scaled up and redesigned the deployment mechanism to work with the larger 14 m CFRP boom dedicated for the Gossamer-2 size spacecraft. In this paper the concept and design of the up-scaled boom deployment mechanism are described, followed by the main part that addresses the environmental testing performed on the prototype of the up-scaled boom deployment unit. The objectives, the test procedure and the results from thermal-vacuum, vibration and functional deployment tests are presented in detail. Furthermore, FE-Analyses for simulating the vibration tests are performed. In this regard the used FE-model is described and the obtained results are shown in detail. Consequently, the simulated and measured results are compared and discussed.

Item URL in elib:https://elib.dlr.de/102096/
Document Type:Conference or Workshop Item (Speech)
Title:Environmental Testing and Analysis of a Boom Deployment Mechanism for Gossamer-2
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Meyer, Sebastiansebastian.meyer (at) dlr.deUNSPECIFIED
Zander, MartinMartin.Zander (at) dlr.deUNSPECIFIED
Straubel, Marcomarco.straubel (at) dlr.deUNSPECIFIED
Hühne, Christianchristian.huehne (at) dlr.deUNSPECIFIED
Date:October 2015
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Unpublished
Keywords:Deployable structures, GOSSAMER-2
Event Title:66th International Astronautical Congress
Event Location:Jerusalem, Israel
Event Type:international Conference
Event Dates:12.-16. Okt. 2015
Organizer:IAF - International Astronautical Federation
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Technology
DLR - Research area:Raumfahrt
DLR - Program:R SY - Technik für Raumfahrtsysteme
DLR - Research theme (Project):R - Entfaltungstechnologie . Solar Sail (old)
Location: Braunschweig
Institutes and Institutions:Institute of Composite Structures and Adaptive Systems > Functional Lightweight Structures
Deposited By: Meyer, Sebastian
Deposited On:13 Jan 2016 16:46
Last Modified:01 Dec 2018 19:52

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