Waveguide-based Dielectric and Magnetic Property Measurement

Materials and Coatings
Waveguide-based Dielectric and Magnetic Property Measurement (GSC-TOPS-371)
Non-destructive characterization of arbitrarily shaped samples
Overview
Understanding the composition of planetary surfaces is crucial for advancing space exploration and preparing for future human missions to the Moon and Mars. NASA’s proposed International Mars Ice Mapping (I-MIM) mission aims to use Synthetic Aperture Radar (SAR) to identify near-surface ice deposits on Mars, which could serve as a vital resource for future explorers. To support this effort, scientists must first determine how radar signals interact with the diverse materials found on these planetary bodies, such as rock, regolith, and buried ice. An understanding of these interactions is critical to designing specialized SARs for such missions, as well as to determining their detection capabilities in specific environments. Traditional methods of analyzing such materials have provided valuable insights, but they often lack the ability to assess the 3-D electromagnetic (EM) properties of rock and soil, which are critical for improving radar-based detection capabilities. Furthermore, existing techniques require regularly shaped samples (e.g., rectangles). Martian and other planetary rock samples brought back to Earth are precious and cannot be altered, eliminating these techniques as an option. Recognizing this challenge, a team of engineers and scientists at NASA’s Goddard Space Flight Center (GSFC) have developed an advanced laboratory-based system for measuring the dielectric and magnetic properties of arbitrarily shaped samples with high accuracy.

The Technology
This NASA invention utilizes a simple waveguide-based measurement system to determine the complex dielectric permittivity and magnetic permeability of arbitrary-shaped planetary rock samples. The system operates at L-band frequencies (~1 GHz) and can be extended to P- and S-bands for broader applications. The approach involves placing an arbitrarily-shaped sample inside an open-ended waveguide excited by a coaxial probe, measuring the scattering parameters, and extracting dielectric and magnetic properties through computational modeling and optimization techniques. A key aspect of this system is its ability to handle non-uniform and irregularly shaped rock samples, enabling the measurement of real-world planetary materials without requiring extensive sample preparation. The methodology includes calibration in an anechoic chamber, computational modeling, and iterative refinement of measured vs. simulated scattering parameters to extract the material properties. Future advancements will involve expanding measurements to different frequency bands, refining computational models using artificial intelligence, and automatically rotating samples within the waveguide to obtain multiple directional measurements (enhancing precision while reducing test time). This NASA innovation has been successfully applied to two Martian meteorite samples, yielding values of dielectric permittivity and permeability relevant for Mars radar applications. The system will further be leveraged to build an expansive database of the dielectric properties of planetary soils and rocks to improve radar-based mapping (e.g., subsurface mapping) missions. The invention could also be applied for the non-destructive screening of a variety of samples using radio waves, including biological samples for medical purposes, additive manufacturing feedstock or finished parts, and mining-related rock samples to test for impurities or resources of interest. This NASA invention is at technology readiness level (TRL) 5 (component and/or breadboard validation in relevant environment) and is available for patent licensing.
An artist illustration depicting the I-MIM mission concept. Low and to the left, an orbiter passes above the Martian surface, detecting buried water ice through a radar instrument and large reflector antenna. Credit: NASA
Benefits
  • Non-destructive measurement: Enables analysis of precious planetary samples without altering their physical state.
  • Applicability to arbitrary shapes: Works with irregularly shaped samples, unlike traditional flat-surface measurement techniques.
  • Adaptable for different frequencies: While initially developed for L-band, the invention can be easily modified for P- and S-band frequencies.
  • Low-cost: This novel technique leverages commercial-off-the-shelf (COTS) components and has low implementation costs.
  • Scalability and automation potential: Potential to be expanded into a semi-automated system for rapid surveying of samples.

Applications
  • Dielectric and magnetic property characterization of planetary samples
  • Planetary radar / SAR system development (e.g., for lunar, Martian, and terrestrial subsurface mapping)
  • Mining and geological surveys (mineral identification & composition analysis; subsurface imaging for resource exploration; rock and soil characterization)
  • Biology & medicine (characterization of biological tissues; non-invasive medical imaging enhancement)
  • Testing of additively manufactured components (dielectric and magnetic property validation of new feedstock materials and printed components)
Technology Details

Materials and Coatings
GSC-TOPS-371
GSC-18965-1
Similar Results
Photo from NASA SESAR paper.
Dual-Polarized, Wideband, Lightweight P-band Antenna Element and Array
The P-band antenna array is built from rows and columns of antenna elements for the purpose of allowing beam steering up to the maximum desirable angle without incurring grating lobes in the radiation patterns. For flexible mission planning, a large array can be built from several of the small, panel-like elements. The elements are deployable from a folded or stacked stowed configuration during launch, arranged side by side during operation. Each antenna element is itself a fully functional small antenna array. The number of panels can be chosen as dictated by the mission objectives and budget. Three geometries were designed and tested. Geometry 1 features non-planar metal structures with minimal dielectric support, where the back cavity is closed. Geometry 2 features non-planar metal structures with minimal composite sheet dielectric support, but with an open cavity. Both geometries avoid large flat sheets, which are vulnerable to bending, thereby increasing the mechanical stiffness of the structure while using only thin sheet metal and maintaining an exceptionally low mass-to-size ratio. Geometry 3 features planar metal structures, with sandwich composite dielectric support and an open cavity. While it does not benefit from the mechanical stiffness utilized in non-planar designs, the planar sandwich structure increase robustness and reduces the cost of fabrication. All element geometries have wideband capabilities and are dual polarized. Although designed for space and planetary exploration, the P-band antenna is also valuable for various terrestrial use cases. The P-band antenna array is at technology readiness level (TRL) 5 (component and/or breadboard validation in relevant environment) and is available for patent licensing.
https://www.flickr.com/photos/gsfc/4691464850
Concept Development for Advanced Spaceborne Synthetic Aperture Radar
The current innovation utilizes heritage flight proven L-band Digital Beamforming Synthetic Aperture Radar (DBSAR) in conjunction with a new P-Band Digital beamforming Polarimetric and Interferometric EcoSAR (ESTO IIP) architecture. The system employs digital beamforming (DBF) and reconfigurable hardware to provide advanced radar capabilities not possible with conventional radar instruments. The SAR is operated without the use of a slewing antenna allowing the single radar system to provide polarimetric imaging, interferometry, and altimetry or scatterometry data types. The SAR is also capable of Sweep-SAR, simultaneous SAR/GNSS-R , and simultaneous active/passive techniques. This system has an increased coverage area and can rapidly image large areas of the surface using the simultaneous left/right imaging. The resulting images maintain their full resolution and allows for faster full coverage mapping
Digital Beamforming Interferometry
Digital Beamforming Interferometry
NASA Goddard Space Flight Center (GSFC) has developed a new approach that uses a single phased array antenna and a single pass configuration to generate interferograms, known as Digital Beamforming Interferometry. A digital beamforming radar system allows the implementation of non-conventional radar techniques, known as Digital Beamforming Synthetic Aperture Radar Multi-mode Operation (DBSAR). DBSAR is an L-Band airborne radar that combines advanced radar technology with the ability to implement multimode remote sensing techniques, including several variations of SAR, scatterometry over multiple beams, and an altimeter mode. The Multiple channel data acquired with a digital beamformer systems allows the synthesis of beams over separate areas of the antenna, effectively dividing the single antenna into two antennas. The InSAR technique is then achieved by generating interferograms from images collected with each of the antennas. Since the technique is performed on the data, it allows for synthesizing beams in different directions (or look angles) and performs interferometry over large areas. Digital Beamforming Interferometry has potential in many areas of radar applications. For example, NASA GSFC innovators developed the first P-Band Digital Beamforming Polarimetric Interferometric SAR Instrument to measure ecosystem structure, biomass, and surface water.
Improved Lunar Regolith Simulant Ion Implantation
Researchers and other technology developers require regolith simulants that accurately emulate the properties of lunar, Martian, and asteroid soils to ensure that the processes, devices, tools, and sensors being developed will be usable in an active mission environment. To move toward higher fidelity regolith simulants, NASA has developed a system that takes typical regolith simulants and implants ions of relevant elements to better simulate the conditions of extraterrestrial soils. The ion implantation device developed here is composed of three key elements as shown in the figure below: two hopper and rotary valve elements and the acceleration grid structure. To perform the ion implantation, the system is first placed within a vacuum chamber, pumped down, and gases of the elements of interest are pumped into the chamber. The system then first passes a mass of granulated lunar regolith simulant through two stages of hoppers and rotary valves to condition the material. Key to the system is a process for interstitial gas removal (a source of contamination) as shown in the figure on the right. After conditioning, the regolith simulant is passed between two parallel electrodes under a high voltage, accelerating ions of the process gas and implanting those ions within the regolith simulant at controllable depths. The related patent is now available to license. Please note that NASA does not manufacturer products itself for commercial sale.
https://science.nasa.gov/mission/viper/
3D Lidar for Improved Rover Traversal and Imagery
The SQRLi system is made up of three major components including the laser assembly, the mirror assembly, and the electronics and data processing equipment (electronics assembly) as shown in the figure below. The three main systems work together to send and receive the lidar signal then translate it into a 3D image for navigation and imaging purposes. The rover sensing instrument makes use of a unique fiber optic laser assembly with high, adjustable output that increases the dynamic range (i.e., contrast) of the lidar system. The commercially available mirror setup used in the SQRLi is small, reliable, and has a wide aperture that improves the field-of-view of the lidar while maintaining a small instrument footprint. Lastly, the data processing is done by an in-house designed processor capable of translating the light signal into a high-resolution (sub-millimeter) 3D map. These components of the SQRLi enable successful hazard detection and navigation in visibility-impaired environments. The SQRLi is applicable to planetary and lunar exploration by unmanned or crewed vehicles and may be adapted for in-space servicing, assembly, and manufacturing purposes. Beyond NASA missions, the new 3D lidar may be used for vehicular navigation in the automotive, defense, or commercial space sectors. The SQRLi is available for patent licensing.
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