1. CornetteE. S. “Forebody Temperatures and Calorimeter Heating Rates Measured During Project Fire II Reentry at 11.35 Kilometers per Second,” NASA TM-X-1389, 1966.
2. CauchonD. L.“Radiative Heating Results from the Fire II Flight Experiment at a Reentry Velocity of 11.4 Kilometers per Second,” NASA TM-X-1402, 1967.
3. SlocumbT. H.Jr. “Project Fire Flight II Afterbody Temperatures and Pressures at 11.35 Kilometres per Second (37 200 Feet per Second),” NASA TM-X-1319, 1966.
4. Progress in Astronautics and Aeronautics;Sutton K.,1985
5. Convective and radiative heat transfer analysis for the Fire II forebody