Lightweight Composite Reflectarray that can be Flattened, Folded, and Coiled for Compact Stowage

Author:

Arya Manan1,Hodges Richard1,Sauder Jonathan F.1,Horst Stephen1,Mobrem Mehran1,Pedivellano Antonio2,Wen Alexander2,Truong Alan2,Pellegrino Sergio2

Affiliation:

1. NASA Jet Propulsion Laboratory

2. California Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Reference16 articles.

1. 2Arya, M., Packaging and Deployment of Large Planar Spacecraft Structures, Ph.D. thesis,California Institute of Technology, 2016.

2. Ultralight Structures for Space Solar Power Satellites

3. Crease-free biaxial packaging of thick membranes with slipping folds

4. Large-Area Deployable Reflectarray Antenna for CubeSats

Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Impact Analysis of Facet Gaps in X-band Origami based Deployable Reflectarray Antenna;2023 IEEE Microwaves, Antennas, and Propagation Conference (MAPCON);2023-12-11

2. Slew Maneuver Constraints for Agile Flexible Spacecraft;Journal of Guidance, Control, and Dynamics;2023-12

3. Structural and Radio Frequency Co-Design and Optimization of Large Deployable Reflectarrays for Space Missions;IEEE Transactions on Antennas and Propagation;2023-05

4. Modeling of Damage in Coilable Composite Shell Structures;AIAA SCITECH 2023 Forum;2023-01-19

5. Slew Maneuver Constraints for Agile Flexible Spacecraft;AIAA SCITECH 2023 Forum;2023-01-19

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