A multilevel interconnect silicon carbide integrated circuit chip with co-fired ceramic package and circuit board recently developed at the NASA GRC Smart Sensors and Electronics Systems Branch for high temperature applications. High temperature silicon carbide electronics and compatible packaging technologies are elements of instrumentation for aerospace engine control and long term inner-solar planet explorations.
Silicon Carbide Integrated Circuit Chip
NASA Glenn technician Ariana Miller prepares an ultrahigh vacuum chamber used to test the materials used in silicon carbide based sensors and electronics that can operate at extremely high temperatures (500 degrees Celsius and higher) for applications such as sensor systems for aircraft engines and Venus exploration.
Clean Room Facility
Laboratory Researcher suits up for work in a research clean room.  Personal Protective Equipment, PPE, Portait Series
engineers fabricate silicon carbide sensors
SILICON CARBIDE GROWTH FACILITY - CLEAN ROOM FACILITY AND SURFACE ANALYTICAL LABS
GRC-1998-C-01261
SILICON CARBIDE GROWTH FACILITY - CLEAN ROOM FACILITY AND SURFACE ANALYTICAL LABS
GRC-1998-C-01254
SILICON CARBIDE GROWTH FACILITY - CLEAN ROOM FACILITY AND SURFACE ANALYTICAL LABS
GRC-1998-C-01262
CP-SiCS Constant Pressure - Silicon Carbide Combustion Synthesis
GRC-2004-C-01034
CP-SiCS Constant Pressure - Silicon Carbide Combustion Synthesis
GRC-2004-C-01022
SILICON CARBIDE GROWTH FACILITY - CLEAN ROOM FACILITY AND SURFACE ANALYTICAL LABS
GRC-1998-C-01260
SILICON CARBIDE GROWTH FACILITY - CLEAN ROOM FACILITY AND SURFACE ANALYTICAL LABS
GRC-1998-C-01255
SILICON CARBIDE GROWTH FACILITY - CLEAN ROOM FACILITY AND SURFACE ANALYTICAL LABS
GRC-1998-C-01250
Silicon Carbide, SiC wafer v8.1 OpAmp Chip in Co-fired Alumina Package for High-temperature Application
GRC-2015-C-00598
Fully Packaged Silicon Carbide Piezoresistive Pressure Transducer that measures pressures at temperature as high as 600 degrees Celsius
GRC-2007-C-02517
Fully Packaged Silicon Carbide Piezoresistive Pressure Transducer that measures pressures at temperature as high as 600 degrees Celsius
GRC-2007-C-02513
Shigehiro Nishino -- Visiting faculty fellow Dr. Shigehiro Nishino introduced the Lewis team to a unique chemical vapor deposition (CVD) strategy to grow silicon carbide crystals on silicon wafers.
CHEMICAL VAPOR DEPOSITION CVD REACTION CHAMBER
Hall Effect Rocket with Magnetic Shielding Technology Development Unit 1 with Large Radiator working in conjunction with High Power 300 Volt Silicon Carbide Power Processing Unit
GRC-2015-C-01182
Photos for Web Feature by Victoria (Tori) Woods; Micro-Electro Mechanical Systems (MEMS) using vacuum technology; fabricating High Temperature Electronics for Harsh Environments using silicon carbide substrates
GRC-2011-C-00579
Hall Effect Rocket with Magnetic Shielding Technology Development Unit 1 with Large Radiator working in conjunction with High Power 300 volt Silicon Carbide Power Processing Unit
Hall Effect Rocket
Phil Neudeck- Can Take the Heat      When it comes to the heat of extreme environments like Venus, electronics can get fried within a few minutes of arrival.  But NASA Researcher Phil Neudeck and his team have developed extremely durable silicon carbide semiconductor integrated circuits to survive those harsh conditions. After successfully testing the electronics in our high-pressure, high-temperature extreme environments chamber, there is now a path forward for Venus landers to survive and operate scientific experiments on the planet’s surface for longer durations.
Phillip Neudeck with Venus Durable Integrated Circuit Electronic
A nickel alloy developed at the National Aeronautics and Space Administration (NASA) Lewis Research Center being poured in a shop inside the Technical Services Building. Materials technology is an important element in the successful development of both advanced airbreathing and rocket propulsion systems. An array of dependable materials is needed to build different types of engines for operation in diverse environments. NASA Lewis began investigating the characteristics of different materials shortly after World War II. In 1949 the materials research group was expanded into its own division. The Lewis researchers studied and tested materials in environments that simulated the environment in which they would operate.    Lewis created two programs in the early 1960s to create materials for new airbreathing engines. One concentrated on high-temperature alloys and the other on cooling turbine blades. William Klopp, Peter Raffo, Lester Rubenstein, and Walter Witzke developed Tungsten RHC, the highest strength metal at temperatures over 3500⁰ F. The men received an IR-100 Award for their efforts. Similarly a cobalt-tungsten alloy was developed by the Fatigue and Alloys Research Branch. The result was a combination of high temperature strength and magnetic properties that were applicable for generator rotor application.    John Freche invented and patented a nickel alloy while searching for high temperature metals for aerospace use. NASA agreed to a three-year deal which granted Union Carbide exclusive use of the new alloy before it became public property.
NASA Lewis Nickel Alloy being Poured in the Technical Service Building