- Author
- Marxman, G. A. | Gilbert, M.
- Title
- Turbulent Boundary Layer Combustion in the Hybrid Rocket.
- Coporate
- United Technology Corp., Sunnyvale, CA
- Sponsor
- Navy Dept., Washington, DC
- Report
- WSS/CI Paper 62-24, 1962, 38 p.
- Contract
- NOW-61-1000-C
- Book or Conf
- Combustion Institute/Western States Section. 1962 Fall Meeting., Sacramento, CA, 1962
- Keywords
- boundary layer combustion | gasification | regression rate
- Identifiers
- hybrid rocket engine; fundamental aspects of the combustion mechanisms