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Meeting 2026 TMS Annual Meeting & Exhibition
Symposium Advanced Materials for Reusable Rocket Engines
Presentation Title Frictional Ignition Testing of Metals in Oxygen up to 24.1 MPa
Author(s) Tim Wabel, Fabio Bendana, Vincent Phong, Andres Garcia Jimenez, Zachary Cordero
On-Site Speaker (Planned) Tim Wabel
Abstract Scope Friction-induced ignition of metals in high-pressure oxygen is a significant risk for liquid-propellant rocket engines. The OXygen Frictional Ignition Research Experiment was developed at The Aerospace Corporation to provide data to assess ignition risks due to frictional heating. The apparatus consists of an optically-accessible oxygen-safe test chamber with a 68.9 MPa (10,000 psi) pressure rating. Within the chamber, two cylindrical samples, one stationary and one rotating at 17,000 rpm, are contacted and axially loaded. The contact load between the samples is increased linearly until either ignition or structural failure (i.e., fracture or plastic deformation) of the sample(s) occur. The relative ignition sensitivity of each material is determined from the product of the contact pressure and sliding surface velocity at ignition. Frictional ignition of several common aerospace alloys has been evaluated over a range of pressures from 3.45 to 24.1 MPa (500 to 3,500 psi) in pure oxygen.
Proceedings Inclusion? Planned:
Keywords Environmental Effects, Iron and Steel,

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Frictional Ignition Testing of Metals in Oxygen up to 24.1 MPa
HVOF Thermal Spray Additively Manufacturing Processing of GRX-810 Alloy for Scalable Rocket Engine Components
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Temperature-Dependent Effects in the Aeroplastic Design of Turbine Disks
Using ICMDŽ Software to Design High Strength, Printable, Burn Resistant Nickel-Based Superalloys for Reusable Rocket Engines
Wire-Arc AM Combustion Chambers: Reusability Considerations with AM and Accelerating the Material Development Path to Flight

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