Analytical evaluation of rocket nozzle ablation
- 29 January 1964
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- THERMAL PERFORMANCE OF HEAT SHIELD COMPOSITES DURING PLANETARY ENTRYPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1963
- Thermal Degradation of a Char-Forming Plastic During Hypsersonic FlightARS Journal, 1962
- Equilibrium Composition of the C/H System at Elevated TemperaturesThe Journal of Chemical Physics, 1962
- An Experimental and Theoretical Study of Quartz Ablation at the Stagnation PointJournal of the Aerospace Sciences, 1960
- On Catalytic Recombination Rates in Hypersonic Stagnation Heat TransferJournal of Jet Propulsion, 1958
- Theory of Stagnation Point Heat Transfer in Dissociated AirJournal of the Aerospace Sciences, 1958