The Deployable Structures group develops novel technologies, mechanisms, and systems to increase the amount of capability delivered to satellites per unit of stowed volume and mass. The team specializes in High-Strain Composite (HSC) [1] based structures for antennas, solar arrays, and other satellite systems. We are seeking researchers who can help advance our efforts in materials science (specifically for HSCs), deployable mechanism design, high-fidelity structural analysis, and antenna design.
In the realm of materials science, we’re working to better understand and estimate characteristics of complex multi-layer, multi-material composite layups that behave non-linearly when structurally loaded. Major areas of interest are listed below, with similar published works referenced. HSC material properties database creation [2], and radiation effects characterization for HSCs [3].
With deployable mechanism design, we’re always looking for new stowage and deployment techniques for varying satellite systems, such as those mentioned above. Emphasis is placed on practical implementation of concepts, and how the structures integrate with the whole satellite. For examples of deployable structure design for satellites, see [4] and [5].
For structural analysis, new techniques are desired to predict behavior, performance, and failure mechanisms in kinematically-complex multi-body systems made up of different materials, including composite materials that behave non-linearly under loading. Major areas of interest are listed below, with similar published works referenced. Multi-scale modeling of composite structures [6], and shock propagation analysis in composite structures [7].
In antenna design, we’re working to develop stowable versions of many antenna types, specifically those with medium to high gain, and in the frequency ranges from L- to Ka-bands. The following references cover relevant work on deployable satellite antennas. See [8], [9], and [10].
References:
[1] Thomas W. Murphey, William Francis, Bruce Davis and Juan M. Mejia-Ariza. "High Strain Composites," AIAA 2015-0942. 2nd AIAA Spacecraft Structures Conference. January 2015.
[2] Loujaine Mehrez, David Moens, Dirk Vandepitte. “Stochastic identification of composite material properties from limited experimental databases, part I: Experimental database construction,” Mechanical Systems and Signal Processing, Volume 27, 2012, Pages 471-483.
[3] Abd El-Hameed, A. M. (2022). “Radiation effects on composite materials used in space systems: a review.” NRIAG Journal of Astronomy and Geophysics, 11(1), Pages 313–324.
[4] Pellegrino, S., S. Kukathasan, G. Tibert, and A. Watt. “Small satellite deployment mechanisms,” Department of Engineering, University of Cambridge, 2000.
[5] Y. Miyazaki. "Deployable Techniques for Small Satellites," Proceedings of the IEEE, vol. 106, no. 3, pp. 471-483, March 2018.
[6] J. Llorca et al., “Multiscale Modeling of Composite Materials: a Roadmap Towards Virtual Testing.” Advanced Materials, vol 23: 5130-5147, October 2011.
[7] James LeBlanc, Arun Shukla, Carl Rousseau, Alexander Bogdanovich. “Shock loading of three-dimensional woven composite materials,” Composite Structures, Volume 79, Issue 3, 2007, Pages 344-355.
[8] J. Costantine et al., "UHF Deployable Helical Antennas for CubeSats," IEEE Transactions on Antennas and Propagation, vol. 64, no. 9, Pages 3752-3759, Sept. 2016.
[9] Cao, W., and Cheng, P. (August 9, 2022). "Design and Kinematic Analysis of a Novel Deployable Antenna Mechanism for Synthetic Aperture Radar Satellites." ASME. J. Mech. Des. November 2022; 144(11): 114502.
[10] Duan, Baoyan, Yiqun Zhang, and Jingli Du. “Large Deployable Satellite Antennas.” Springer Singapore, 2020.