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2. 2Cornette, E. S. “Forebody Temperatures and Calorimeter Heating Rates Measured During Project Fire II Reentry at 11.35 Kilometers Per Second,” Tech. Rep. NASA TM X-1305, Langley Research Center, 1966.
3. 3Cauchon, D. L., McKee, C. W., and Cornette, E. S. “Radiative Heating Results from the Fire II Flight Experiment at a Reentry Velocity of 11.4 Kilometers per Second,” Tech. Rep. NASA TM X-1402, Langley Research Center, 1967.
4. Monte Carlo simulation of radiating re-entry flows
5. Nonequilibrium radiation during re-entry at 10 km/s