- 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