Sensatek Propulsion Technology, Inc. proposes to demonstrate the feasibility of a wireless, passive, nanoparticle-based sensor system. The sensor in its current form can be used to measure real time temperatures and pressures wirelessly without the need of an external energy source. It should be noted that the same sensing principle can be used for strain monitoring as well. It comprises of a microwave-resonator-based sensor, a microwave transceiver, and a custom-made antenna. The microwave-resonator-based sensors uses a dielectric resonator structure, a low-profile reflective patch temperature sensor, and a pressure sensor based on evanescent-mode resonator structure. These sensors are made of high-temperature-stable and corrosion-resistant ceramic materials which are suitable for extreme-environment applications. The use of nanoparticles can further reduce the size of the sensor enabling deployment in current hard-to-access areas. This approach will enable not only surface measurements of pressure and temperature but also provide in-flow measurements of gas path flows at cryogenic and high temperature environments. In-flow measurements within the metal piping of the fluid systems helps provide a dynamic and real time analysis of the operations of the system. Besides, the embedded sensor helps in keeping the structural integrity of the component intact since its installation doesnt require machining pathways as is needed for traditional sensor cables. The proposed innovation will specifically provide the following benefits for propulsion system test, development & flight applications: Reduced cabling costs/time Reduced auxiliary power requirements Reduced weight penalties/operational costs associated with cabling and auxiliary power components Remote, real-time monitoring of component health Flexible application due to low profile of sensor Extreme environment measurement & survivability Potential NASA Applications -Reduced cost and labor requirements associated with instrumentation installation at 8-Foot High-Temperature Tunnel Facility for National Aerospace Plan Concept Demonstration Engine, X43 Hyper-X engine -Reduce operational costs for various engine test-beds, developmental & launch facilities at SSC, GRC, MSFC and KSC Propulsion Systems Laboratory -Structural health monitoring into the numerous NASA programs particularly the RS-25 engines on SLS. Potential Non-NASA Applications Monitoring of harsh environments in inaccessible locations provides insight to increase the reliability and efficenciy in systems that includes: HyFly Dual Combustor Ramjet Engine, X43C programs Ground Demonstrator, Air Force Research Laboratorys SJX611 and SJX612 engines; Power Generation & Aviation Gas Turbine Engines for Maintenance & Operational Monitoring; Automotive for Continuous Monitoring for Component Health Indication; and Chemical Plants for Process Control, Safety & Automation.
