Major research outcome
- Prof. Jae-Hung Han, Origami-based Deployable Space Shelter
- 관리자 |
- 2023-12-26 16:42:52|
- 109
- 2023-12-26 16:42:52|
With recent advancements in launch vehicle technology, the scope of space missions, including deep space exploration and manned missions, has expanded. However, the space environment possesses various critical hazards, such as high-energy cosmic radiation and high-speed collisions with micrometeoroids, which can be fatal to astronauts and equipment. Therefore, for sustainable and long-term manned missions, a space shield structure or space shelter is indispensable. Yet, there are no precedents of actual space shelter utilized on the Moon or Mars, and its development remains a challenging task. The primary obstacle arises from the conflict between the size constraint imposed by launch vehicles for transportation and the requirement for thick materials and large-scale construction for effective protection performance. In addition, the previously proposed concepts may not be practical as an initial space shelter since they require a lot of time and resources for installation and construction.
While origami technique, capable of transforming structures' shapes, sizes, and mechanical properties through systematic folding of thin sheets, is applied to various applications such as robots, space structures, and architecture. However, physical implementation and deployment of large structures with origami techniques is considerably complex and challenging. It is because typical large-scale origami designs with thin-paneled structures are prone to deformation under load, structurally vulnerable, and can become unstable during deployment. On the other hand, if the panel becomes thick, the deployment motion is limited due to interference between panels. To address this, the pattern should be modified in an intricate manner, ultimately complicating the deployment process.
To overcome the limitations of conventional space shelter concepts, Smart Structures and H/W Systems Laboratory (SSHS), led by Professor Jae-Hung Han in the Department of Aerospace Engineering at KAIST, has developed a deployable structure design suitable for early space habitats or shelters, based on origami techniques (see Figure 1). Unlike traditional origami patterns, the proposed design concept allows the use of thick panels while enabling efficient transport, excellent protection performance, and rapid and simple deployment mechanism.
Figure 1. Conceptual figure of Origami-based Deployable Space Shelters
The foundational pattern for the deployable space shelter design, as illustrated in Figure 2-a, allows folding with a single plane, resulting in a final shape surrounded by pyramidal sides. The proposed pattern enables adjustments to the final shape and available internal volume according to design parameters. It can be folded into a flat shape, while panels do not deform during the deployment process, enabling the application of thick and rigid panels (see Figure 2-b). Moreover, it is suitable for a large-scale shelter since the presented design is scalable according to panel thickness and structure size.
Deployment of proof-of-concept model (GIF)
Figure 2. Foundational pattern for the deployable space shelter
(a) Various patterns and operational shapes, (b) Folding process of paper model and thick-paneled model
The designed deployable space shelter enables efficient transport via launch vehicles due to its compact stowed shape. When considering the payload space of SpaceX's Falcon-9 launch vehicle, if the deployable space shelter is composed of 30mm thick panel, and its dimensions are approximately 2m in height and 5m in diameter in operational state, a total of 20 or more units can be transported at once.
Figure 3. Efficient storage of multiple shelters in one launch vehicle (Launch vehicle image credit: SpaceX)
The novel concept of space shelter presented in this study is expected to pave new dimensions for the essential development of space habitat structures for future space missions. Further validation is planned through the creation with large-scale models to demonstrate its feasibility in actual space missions.
While origami technique, capable of transforming structures' shapes, sizes, and mechanical properties through systematic folding of thin sheets, is applied to various applications such as robots, space structures, and architecture. However, physical implementation and deployment of large structures with origami techniques is considerably complex and challenging. It is because typical large-scale origami designs with thin-paneled structures are prone to deformation under load, structurally vulnerable, and can become unstable during deployment. On the other hand, if the panel becomes thick, the deployment motion is limited due to interference between panels. To address this, the pattern should be modified in an intricate manner, ultimately complicating the deployment process.
To overcome the limitations of conventional space shelter concepts, Smart Structures and H/W Systems Laboratory (SSHS), led by Professor Jae-Hung Han in the Department of Aerospace Engineering at KAIST, has developed a deployable structure design suitable for early space habitats or shelters, based on origami techniques (see Figure 1). Unlike traditional origami patterns, the proposed design concept allows the use of thick panels while enabling efficient transport, excellent protection performance, and rapid and simple deployment mechanism.
Figure 1. Conceptual figure of Origami-based Deployable Space Shelters
The foundational pattern for the deployable space shelter design, as illustrated in Figure 2-a, allows folding with a single plane, resulting in a final shape surrounded by pyramidal sides. The proposed pattern enables adjustments to the final shape and available internal volume according to design parameters. It can be folded into a flat shape, while panels do not deform during the deployment process, enabling the application of thick and rigid panels (see Figure 2-b). Moreover, it is suitable for a large-scale shelter since the presented design is scalable according to panel thickness and structure size.
Deployment of proof-of-concept model (GIF)
Figure 2. Foundational pattern for the deployable space shelter
(a) Various patterns and operational shapes, (b) Folding process of paper model and thick-paneled model
The designed deployable space shelter enables efficient transport via launch vehicles due to its compact stowed shape. When considering the payload space of SpaceX's Falcon-9 launch vehicle, if the deployable space shelter is composed of 30mm thick panel, and its dimensions are approximately 2m in height and 5m in diameter in operational state, a total of 20 or more units can be transported at once.
Figure 3. Efficient storage of multiple shelters in one launch vehicle (Launch vehicle image credit: SpaceX)
The novel concept of space shelter presented in this study is expected to pave new dimensions for the essential development of space habitat structures for future space missions. Further validation is planned through the creation with large-scale models to demonstrate its feasibility in actual space missions.
| Attach File |
|---|