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Verification Testing of the Gossamer-1 Deployment Demonstrator

Seefeldt, Patric and Spröwitz, Tom and 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), 26-30 Sep 2016, Guadalajara, Mexico. ISBN 9781510835825.

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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.

Item URL in elib:https://elib.dlr.de/106399/
Document Type:Conference or Workshop Item (Speech)
Title:Verification Testing of the Gossamer-1 Deployment Demonstrator
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Seefeldt, PatricUNSPECIFIEDhttps://orcid.org/0000-0002-2067-9458UNSPECIFIED
Spröwitz, TomUNSPECIFIEDhttps://orcid.org/0000-0001-5369-6919UNSPECIFIED
Grundmann, Jan ThimoUNSPECIFIEDhttps://orcid.org/0000-0002-8809-0981UNSPECIFIED
Journal or Publication Title:Proceedings of the 67th International Astronautical Congress
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In ISI Web of Science:No
Keywords:deployment systems, deployable structures, deployable membranes, verification testing, mechanisms, solar sailing
Event Title:67th Internationa Astronautical Congress (IAC)
Event Location:Guadalajara, Mexico
Event Type:international Conference
Event Dates:26-30 Sep 2016
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space System Technology
DLR - Research area:Raumfahrt
DLR - Program:R SY - Space System Technology
DLR - Research theme (Project):R - Entfaltungstechnologie . Solar Sail (old)
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Mechanic and Thermal Systems
Deposited By: Sznajder, Dr.-Ing. Maciej
Deposited On:05 Oct 2016 15:09
Last Modified:29 Mar 2023 00:28

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