Maria Sakovsky
Assistant Professor of Aeronautics and Astronautics
Web page: https://reactlab.stanford.edu/
Bio
Maria Sakovsky's work focuses on the use of shape adaptation to realize space structures with reconfigurable geometry, stiffness, and even non-mechanical performance (ex. electromagnetic, optical). Particular focus is placed on the mechanics of thin fiber reinforced composite structures, the interplay between composite material properties and structural geometry, as well as embedded functionality and actuation of lightweight structures. The work has led to applications in deployable space structures, reconfigurable antennas, and soft robotics.
Maria Sakovsky received her BSc in Aerospace Engineering from the University of Toronto. Following this, she completed her MSc and PhD in Space Engineering at Caltech, where she developed a deployable satellite antenna based on origami concepts utilizing elastomer composites. She concurrently worked with NASA’s Jet Propulsion Laboratory on developing cryogenically rated thin-ply composite antennas for deep space missions. For her ongoing research on physically reconfigurable antennas, she was awarded the ETH Zürich postdoctoral fellowship as well as the Innovation Starting Grant.
Program Affiliations
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Stanford SystemX Alliance
2024-25 Courses
- Introduction to Mechanics of Composite Materials
AA 156 (Spr) - Large Spacecraft Structures
AA 114Q (Win) - Spacecraft Design
AA 236A (Aut) -
Independent Studies (6)
- Directed Research and Writing in Aero/Astro
AA 190 (Aut, Win, Spr, Sum) - Experimental Investigation of Engineering Problems
ME 392 (Aut, Win, Spr, Sum) - Independent Study in Aero/Astro
AA 199 (Aut, Win, Spr, Sum) - Ph.D. Research Rotation
ME 398 (Aut, Spr) - Practical Training
AA 291 (Aut, Win, Spr, Sum) - Problems in Aero/Astro
AA 290 (Aut, Win, Spr)
- Directed Research and Writing in Aero/Astro
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Prior Year Courses
2023-24 Courses
- Introduction to Mechanics of Composite Materials
AA 156 (Spr) - Large Spacecraft Structures
AA 114Q (Aut) - Spacecraft Design Laboratory
AA 236B (Win)
2022-23 Courses
- Introduction to Mechanics of Composite Materials
AA 156 (Spr) - Large Spacecraft Structures
AA 114Q (Aut) - Spacecraft Design Laboratory
AA 236B (Win)
2021-22 Courses
- Large Spacecraft Structures
AA 114Q (Spr)
- Introduction to Mechanics of Composite Materials
Stanford Advisees
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Doctoral Dissertation Advisor (AC)
Catherine Catrambone, Kai Jun Chen, Enquan Chew -
Master's Program Advisor
Sidharth Anantha, Melanny Garcia, Yong Lin He, Thomas Huang, Samuel Montagut Agudelo, Jacob Mukobi, Aditi Pattabhiraman, Cruz Soto -
Doctoral (Program)
Colton Crosby, Sevan Vlieghe
All Publications
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Kinematics-driven design of reconfigurable bistable hinges with high stiffness and stability
MATERIALS & DESIGN
2024; 244
View details for DOI 10.1016/j.matdes.2024.113154
View details for Web of Science ID 001282565100001
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Dynamically reprogrammable stiffness in gecko-inspired laminated structures
SMART MATERIALS AND STRUCTURES
2024; 33 (1)
View details for DOI 10.1088/1361-665X/ad142d
View details for Web of Science ID 001128964700001
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Multistable Structures for Deployable and Reconfigurable Antennas
IEEE. 2024
View details for Web of Science ID 001215536203169
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A multi-stable deployable quadrifilar helix antenna with radiation reconfigurability for disaster-prone areas.
Nature communications
2023; 14 (1): 8511
Abstract
In disaster-prone areas, damaged infrastructure requires impromptu communications leveraging lightweight and adaptive antennas. Accordingly, we introduce a bi-stable deployable quadrifilar helix antenna that passively reconfigures its radiation characteristics in terms of pattern and polarization. The proposed structure is composed of counter-rotating helical strips, connected by rotational joints to allow a simultaneous change in the helix height and radius. Each helical strip is composed of a fiber-reinforced composite material to achieve two stable deployed states that are self-locking. The reconfiguration between an almost omnidirectional pattern and a circularly polarized directive pattern enables the antenna to be suitable for both terrestrial and satellite communication within the L-band. More specifically, the presented design in infrastructure-less areas achieves satellite localization with directive circularly polarized waves and point-to-point terrestrial connectivity with an almost omnidirectional state. Hence, we present a portable, agile, and passively reconfigured antenna solution for low-infrastructure areas.
View details for DOI 10.1038/s41467-023-44189-9
View details for PubMedID 38129404
View details for PubMedCentralID 10056457
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Electromagnetic Reconfiguration Using Stretchable Mechanical Metamaterials.
Advanced science (Weinheim, Baden-Wurttemberg, Germany)
2023: e2203376
Abstract
Response to environmental thermomechanical inputs in applications that range from wearable electronics to aerospace structures necessitates agile communication systems driven by reconfigurable electromagnetic structures. Antennas in these systems must dynamically preserve acceptable radiation characteristics while enabling on-demand performance reconfiguration. However, existing reconfiguration mechanisms through stretchable conductors rely on high-strain behavior in soft substrates, which limits their applicability. Herein, this work demonstrates the use of mechanical metamaterials for stretchable conductors and dielectrics in antennas. Metamaterials allow conductor stretching up to 30% with substrate base material tensile moduli ranging from 26 MPa to 44 GPa. It is shown, through several antenna designs, that mechanical metamaterials enable similar frequency reduction upon stretching as monolithic conductors, while simultaneously providing a miniaturization effect. The conductor patterning, furthermore, provides control over coupling between mechanical stretching and electromagnetic reconfiguration. This approach enables designing reconfigurable antenna functionality through metamaterial geometry in response to arising needs in applications ranging from body-adapted electronics to space vehicles.
View details for DOI 10.1002/advs.202203376
View details for PubMedID 36599682
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Thin ply composite materials with embedded functional elements for cryogenic environments
MATERIALS LETTERS
2023; 330
View details for DOI 10.1016/j.matlet.2022.133201
View details for Web of Science ID 000863107200007
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A Highly Multi-Stable Meta-Structure via Anisotropy for Large and Reversible Shape Transformation.
Advanced science (Weinheim, Baden-Wurttemberg, Germany)
2022: e2202740
Abstract
Shape transformation offers the possibility of realizing devices whose 3D shape can be altered to adapt to different environments. Many applications would profit from reversible and actively controllable shape transformation together with a self-locking capability. Solutions that combine such properties are rare. Here, a novel class of meta-structures that can tackle this challenge is presented thanks to multi-stability. Results demonstrate that the multi-stability of the meta-structure is strictly tied to the use of highly anisotropic materials. The design rules that enable large-shape transformation, programmability, and self-locking are derived, and it is proven that the shapes can be actively controlled and harnessed to realize inchworm-inspired locomotion by strategically actuating the meta-structure. This study provides routes toward novel shape adaptive lightweight structures where a metamaterial-inspired assembly of anisotropic components leads to an unforeseen combination of properties, with potential applications in reconfigurable space structures, building facades, antennas, lenses, and softrobots.
View details for DOI 10.1002/advs.202202740
View details for PubMedID 35861407
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A thin -shell shape adaptable composite metamaterial
COMPOSITE STRUCTURES
2020; 246
View details for Web of Science ID 000540216500004