1. N. A. Anfimov and A. N. Rumynskii, “Radiant-Convective Heat Transfer and Thermal Protection of the Spacecraft Landing on the Surface of the Earth and Other Planets of Solar System,” in: Problems of Mechanics and Heat Transfer in Space Engineering [in Russian] (Moscow, Mashinostroenie, 1982), p. 54.
2. D. B. Lee, J. J. Bertin, and W. D. Goodrich, “Heat Transfer Rate and Pressure Measurements Obtained during Apollo Orbital Entries,” NASA TN D-6028 (1970).
3. D. B. Lee and W. D. Goodrich, “Heat Transfer Environment of the Apollo Command Module during Apollo Superorbital Entry,” NASA TN D-6792 (1972).
4. E. R. Hilje, “Entry Aerodynamics of Lunar Return Conditions Obtained from the Flight of Apollo-4 (AS-501),” NASA TN D-5399 (1969).
5. D. B. Lee, “Apollo Experience Report—Aerothermodynamics Evaluation,” NASA TN D-6843 (1972).