An aerothermochemical analysis of carbon-carbon nozzle regression insolid-propellant rocket motors
- 11 July 1988
- conference paper
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Bulk graphite nozzle recession—an analysis based on the carbon-steam reactionCarbon, 1986
- A Review of Roughness-Induced Nosetip TransitionAIAA Journal, 1983
- Kinetic reaction rates for consumption of pyrolytic graphite by combustion gasesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- A method for computing roughwall heat transfer rates on reentry nosetipsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- The calculation of low-Reynolds-number phenomena with a two-equation model of turbulenceInternational Journal of Heat and Mass Transfer, 1973
- Erosion of graphite in solid-propellant combustion gases and effects on heat-transferAIAA Journal, 1965