Carbonaceous Deposits in a Fuel-Film Cooled Rocket Combustor: Electron Microscopy

Abstract
The high gas–side heat transfer coefficients expected in high-pressure oxygen-rich staged combustion kerosene–oxygen engines require fuel–film cooling in parallel with regenerative cooling to keep ...
Funding Information
  • Science, Mathematics, and Research for Transformation (SMART) Scholarship (N/A)
  • Air Force Small Business Technology Transfer (FA9300-17-C-2501)

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