Deployable structure
A deployable structure is a structure that can change shape so as to significantly change its size.[1][2]
Examples of deployable structures are umbrellas, some tensegrity structures, bistable structures, some Origami shapes and scissor-like structures. Deployable structures are also used on spacecraft for deploying solar panels and solar sails.
Space-based deployable structures can be categorized into three primary classes: the first is the articulated structure class wherein rigid members contain sliding contact joints or are folded at hinge points and pivot to deploy, often locking into place. The second class consists of on-orbit assembly where a device is fabricated and/or mechanically joined in space to form the structure. The final class is high strain structures (often composed of High strain composites) wherein the device is dramatically flexed from one configuration to another during deployment.
Gallery
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Scissor-type structure
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Multiple scissor-type structure
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Simple Hoberman mechanism
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Compound Hoberman mechanism
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Outward folding deployable ring structure
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Inward folding deployable ring structure
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NuSTAR mast in the stowed configuration.
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NuSTAR mast deployed.
See also
[edit | edit source]- Engineering mechanics
- Four-bar linkage
- Kinematics
- Linkage (mechanical)
- Machine
- Outline of machines
- Overconstrained mechanism
- Parallel motion
- Slider-crank linkage
- Compliant mechanism
References
[edit | edit source]- ^ S. Pellegrino (Ed.), Deployable Structures, CISM International Center for Mechanical Sciences, Springer, 2002
- ^ Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
External links
[edit | edit source]- Error creating thumbnail: File missing Media related to Lua error in Module:Commons_link at line 62: attempt to index field 'wikibase' (a nil value). at Wikimedia Commons
- University of Cambridge Deployable structures department publications
