peer-reviewedStructures used in space applications demand the highest levels of stiffness for their mass whilst also performing in a hostile environment. To partly address these requirements and so as to also pack efficiently for stowage during launch we propose a new type of compact telescopic morphing lattice space boom. This boom stows within a 1U CubeSat volume and is lightweight being only 0.4 kg. The boom has a total length of 2 m in its deployed state which is 20 times its stowed height. The device comprises two multi-stable cylindrical composite lattices that are joined telescopically. These lattices nest inside one another in the stowed configuration, with the objective of improving packaging efficiency. Notably, prestress and lami...
Large and ultra-light space structures on base of deployable components will gain in importance for ...
The current barrier to CubeSat proliferation is their lack of utility depth. These small satellites ...
One of the key challenges for small satellites is packaging and reliable deployment of structural bo...
Structures used in space applications demand the highest levels of stiffness for their mass whilst a...
peer-reviewedMorphing composites are relatively new types of structure that change their shape due t...
For advanced space missions, meeting the concurrent requirements of increasing payload size while mi...
peer-reviewedDeployable spacecraft technology should be both lightweight and compact for storage whi...
A larger, stronger deployable boom was developed to handle the requirements of larger, heavier paylo...
peer-reviewedMorphing composites have the potential to significantly reduce the mass and volume of ...
The concept of utilizing small satellites to perform big mission objectives has grown from a distant...
Large deployable lightweight structures development plays a key role for a number of future space ap...
This paper presents a 1 m long self-deployable boom that could be folded around a spacecraft. Previo...
Rationale for the inclusion of deployable structures onboard small satellites is ever increasing. Fo...
Inflatable structures offer the potential of compactly stowing lightweight structures, which assume ...
A new deployable and retractable telescoping boom capable of high deployed stiffness and strength is...
Large and ultra-light space structures on base of deployable components will gain in importance for ...
The current barrier to CubeSat proliferation is their lack of utility depth. These small satellites ...
One of the key challenges for small satellites is packaging and reliable deployment of structural bo...
Structures used in space applications demand the highest levels of stiffness for their mass whilst a...
peer-reviewedMorphing composites are relatively new types of structure that change their shape due t...
For advanced space missions, meeting the concurrent requirements of increasing payload size while mi...
peer-reviewedDeployable spacecraft technology should be both lightweight and compact for storage whi...
A larger, stronger deployable boom was developed to handle the requirements of larger, heavier paylo...
peer-reviewedMorphing composites have the potential to significantly reduce the mass and volume of ...
The concept of utilizing small satellites to perform big mission objectives has grown from a distant...
Large deployable lightweight structures development plays a key role for a number of future space ap...
This paper presents a 1 m long self-deployable boom that could be folded around a spacecraft. Previo...
Rationale for the inclusion of deployable structures onboard small satellites is ever increasing. Fo...
Inflatable structures offer the potential of compactly stowing lightweight structures, which assume ...
A new deployable and retractable telescoping boom capable of high deployed stiffness and strength is...
Large and ultra-light space structures on base of deployable components will gain in importance for ...
The current barrier to CubeSat proliferation is their lack of utility depth. These small satellites ...
One of the key challenges for small satellites is packaging and reliable deployment of structural bo...