Tape springs are straight, thin-walled strips with a curved cross-section. Following recent proposals for large deployable structures exploiting the structural simplicity and robustness of such springs as deployment actuators, the paper investigates the dynamic deployment of a tape spring that is either coiled around a circular hub, or folded into a zig-zag pattern. It is shown that in both cases the spring deforms by forming an elastically deformed region with zero transverse curvature and uniform longitudinal curvature. The process of formation and growth of a fold belongs to a wide class of propagating instabilities. It is characterized by a high peak moment and a lower propagation moment. A compact characterization of the moment{rotatio...
Coiled deployable booms have seen a wide variety of uses both in space and terrestrial applications....
Deployable structures are required for many satellite operations, to deploy booms for communications...
One of the most significant drivers in satellite design is the minimization of mass, in the attempt ...
Tape springs have been used for many years in deployable booms and space mechanisms and currently ar...
Tape springs, defined as thin metallic strips with an initially curved cross-section, are an attract...
International audienceThis work is devoted to the study of tape springs behaviour. We focus on the i...
International audienceIn the framework of deployable structures, we focus on the modeling of tape sp...
This paper presents an experimental and numerical study of the folding, stowage, and deployment beha...
Thin shells made of high modulus material are widely used as lightweight deployable space structures...
One of the most significant drivers in satellite design is the minimization of mass to reduce the la...
Deployable structures are required for many satellite operations, to deploy booms for communications...
International audienceThis paper is focused on the modeling of rod-like elastic bodies that have an ...
Tape springs are being used with increasing frequency in today’s space industry to deploy small sate...
In order to increase the production of power on small satellites, solar panels are commonly deployed...
International audienceThis work is focused on the modeling of rod-like elastic bodies with thin-wall...
Coiled deployable booms have seen a wide variety of uses both in space and terrestrial applications....
Deployable structures are required for many satellite operations, to deploy booms for communications...
One of the most significant drivers in satellite design is the minimization of mass, in the attempt ...
Tape springs have been used for many years in deployable booms and space mechanisms and currently ar...
Tape springs, defined as thin metallic strips with an initially curved cross-section, are an attract...
International audienceThis work is devoted to the study of tape springs behaviour. We focus on the i...
International audienceIn the framework of deployable structures, we focus on the modeling of tape sp...
This paper presents an experimental and numerical study of the folding, stowage, and deployment beha...
Thin shells made of high modulus material are widely used as lightweight deployable space structures...
One of the most significant drivers in satellite design is the minimization of mass to reduce the la...
Deployable structures are required for many satellite operations, to deploy booms for communications...
International audienceThis paper is focused on the modeling of rod-like elastic bodies that have an ...
Tape springs are being used with increasing frequency in today’s space industry to deploy small sate...
In order to increase the production of power on small satellites, solar panels are commonly deployed...
International audienceThis work is focused on the modeling of rod-like elastic bodies with thin-wall...
Coiled deployable booms have seen a wide variety of uses both in space and terrestrial applications....
Deployable structures are required for many satellite operations, to deploy booms for communications...
One of the most significant drivers in satellite design is the minimization of mass, in the attempt ...