Advances in Space Research · 2020 · 25 citations · 9 references
EngineeringAerospace EngineeringMechanical EngineeringAerospace StructuresPropulsionSpacecraft DesignDeployable MechanismsMembrane Module DesignSpacecraft StructuresActive Deployment MechanismsDeployable BoomsDeployable Space StructuresDeployable StructuresDeploymentPayload Deployment MechanismsPerformance Requirements AnalysisSolar Sail Dynamics
For precursor solar sail activities a strategy for a controlled deployment of large membranes was developed based on a combination of zig-zag folding and coiling of triangular sail segments spanned between crossed booms. This strategy required four autonomous deployment units that were jettisoned after the deployment is completed. In order to reduce the complexity of the system an adaptation of that deployment strategy is investigated. A baseline design for the deployment mechanisms is established that allows the deployment actuation from a central bus system in order to reduce the complexity of the system. The mass of such a sail craft will be slightly increased but its performance is still be reasonable for first solar sail missions. The presented design will be demonstrated on breadboard level showing the feasibility of the deployment strategy. The characteristic acceleration will be evaluated and compared to the requirements of certain proposed solar sail missions.
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Proceedings of the 7th European Conference on Space Debris
Tim Flohrer, Fredric H. Schmitz · 2017 · 123 citations
MASCOT—The Mobile Asteroid Surface Scout Onboard the Hayabusa2 Mission
Tra‐Mi Ho, Christian Grimm, Jan Thimo Grundmann et al. · Space Science Reviews · 2016 · 117 citations · Full text
Judit Slíz‐Balogh, András Barta, Gábor Horváth · Monthly Notices of the Royal Astronomical Society · 2018 · 30 citations · Full text
Natural Sciences, Astronomy, Physics +12