HRL Laboratories developed the ceramic materials with hypersonic flight in mind, as they can withstand the extreme environments and high temperatures that hypersonic flight requires. The Aerospace Systems Directorate’s scientists began assessing the potential of HRL’s materials while searching for new thermocouple radiation shields. The SiOC materials were produced through an additive manufacturing process using a pre-ceramic resin. After the part is manufactured, it is subject to a heat treatment that converts it into a fully ceramic state.
“If a material can withstand those temperatures – roughly 3,200 degrees Fahrenheit – it could be used for hypersonic aircraft engine components like struts or flame holders,” said Jamie Szmodis, a hypersonic research engineer with the Aerospace Systems Directorate.
To get an idea of what hypersonic speed is, consider that current aircraft fly at Mach 1, or more than 768 miles per hour. That’s supersonic speed. Hypersonic speed exceeds Mach 5, meaning that aircraft would be flying at speeds of over 4,000 miles per hour. This would allow for faster military response times, more advanced weapons and much faster travel for both the military and commercial sectors.
The CRADA-MTA is a type of technology transfer agreement that allows for the transfer of materials for testing, meaning that the Air Force can now access HRL Laboratories’ ceramic materials for research purposes.
“Without the material transfer agreement, we would have purchased the samples to test them. We would have been a customer, as opposed to a collaborator,” said Szmodis. “With the agreement we are able to provide test results to HRL and provide feedback that is valuable to both parties.”
Under the agreement, the Aerospace Systems Directorate received five thermocouple radiation shields and 15 sample cylinders manufactured from the SiOC resin. Szmodis established a small team from various directorates and specialties to conduct the tests. Scientists from the AFRL Materials and Manufacturing Directorate, Structural Materials Division, Composite Branch, led by Dr. Matthew Dickerson, conducted materials analysis and heat treatments. The Aerospace Systems Directorate, Aerospace Vehicle Division, Structural Validation Branch scientists, led by Bryan Eubanks, performed mechanical analysis focusing on thermal expansion analysis at temperatures ranging from 500 – 3,500ºF. Scientists at the Arnold Engineering Development Complex’s Propulsion Research Facility performed analysis of the material’s characteristics in a high-enthalpy instrumentation test facility.

A sample of additively manufactured silicon oxycarbide (SiOC) material is tested at Arnold Air Force Base. [Image: Air Force]
“The extreme temperature testing that AFRL performed revealed the limits of our new material and challenged us to improve it,” said Dr. Tobias Schaedler, a senior scientist from HRL.
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[Source: Air Force]
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