High-Temperature Heterogeneous Reaction Kinetics of Tungsten Oxidation by CO2, CO, and O2

Author:

Sabourin Justin L.1,Yetter Richard A.1

Affiliation:

1. Pennsylvania State University, University Park, Pennsylvania 16802

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Reference38 articles.

1. Opeka, M. M. "Thermodynamic-Based Materials Selection for Corrosion-Resistant Performance in High-Temperature Missile Propulsion Systems. Part 1. Consideration of Condensed Phase Equilibria," Proceedings of Electrochemical Society, Vol. 2004-16, 2004, pp.253-267.

2. Graphite Rocket Nozzle Erosion Rate Reduction by Boundary-Layer Control Using Ablative Materials

3. Nozzle Throat Erosion Characterization Study Using a Solid-Propellant Rocket Motor Simulator

4. Chemical Erosion of Refractory Metal Nozzle Inserts in Solid-Propellant Rocket Motors

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