This paper considers a lightweight boom with an integral hinge consisting of a thin-walled tube made of carbon fibre reinforced plastic with two longitudinal slots. The dynamic deployment of this boom is studied both experimentally and by means of detailed finite-element simulations. The deployment of the boom can be divided into three phases: deployment; incomplete latching, buckling of the tape springs and large rotation of the boom; and vibration of the boom in latched configuration. The simulations show that the most critical phase is the second one, as the highest strains in both the fibres and the matrix occur at this stage. Through the simulations it is found that the deployment of the particular boom design studied in this paper is ...
Deployable structures made from ultrathin composite materials can be folded elastically and are able...
For advanced space missions, meeting the concurrent requirements of increasing payload size while mi...
The necessity of deployable mechanisms in the field of aerospace is inevitable due to volume limitat...
This paper considers a lightweight boom with an integral hinge consisting of a thin-walled tube made...
An experimental and numerical study of the dynamic deployment of stored strain energy deployable boo...
An experimental and numerical study of the dynamic deployment of stored strain energy deployable boo...
Deployable structures made from ultra-thin composite materials can be folded elastically and are abl...
This paper presents a 1 m long self-deployable boom that could be folded around a spacecraft. Previo...
This work presents an analysis and validation of a foldable boom actuated by tape-spring foldable el...
This paper presents a detailed study of the folding and deployment of a slotted tube hinge made from...
Recently developed analysis techniques for thin shells that can be folded elastically and are able t...
Recently developed analysis techniques for thin shells that can be folded elastically and are able t...
This paper presents an optimization study of a lightweight hinge consisting of a thin walled tube ma...
Thin composite boom structures find large applications in erospace systems such as satellites, deep ...
Thin-walled deployable composite structures with high strain ability are of considerable interest an...
Deployable structures made from ultrathin composite materials can be folded elastically and are able...
For advanced space missions, meeting the concurrent requirements of increasing payload size while mi...
The necessity of deployable mechanisms in the field of aerospace is inevitable due to volume limitat...
This paper considers a lightweight boom with an integral hinge consisting of a thin-walled tube made...
An experimental and numerical study of the dynamic deployment of stored strain energy deployable boo...
An experimental and numerical study of the dynamic deployment of stored strain energy deployable boo...
Deployable structures made from ultra-thin composite materials can be folded elastically and are abl...
This paper presents a 1 m long self-deployable boom that could be folded around a spacecraft. Previo...
This work presents an analysis and validation of a foldable boom actuated by tape-spring foldable el...
This paper presents a detailed study of the folding and deployment of a slotted tube hinge made from...
Recently developed analysis techniques for thin shells that can be folded elastically and are able t...
Recently developed analysis techniques for thin shells that can be folded elastically and are able t...
This paper presents an optimization study of a lightweight hinge consisting of a thin walled tube ma...
Thin composite boom structures find large applications in erospace systems such as satellites, deep ...
Thin-walled deployable composite structures with high strain ability are of considerable interest an...
Deployable structures made from ultrathin composite materials can be folded elastically and are able...
For advanced space missions, meeting the concurrent requirements of increasing payload size while mi...
The necessity of deployable mechanisms in the field of aerospace is inevitable due to volume limitat...