1. U.S. Standard Atmosphere , 1976, NOAA-S/T 76–1562, National Oceanic and Atmospheric Administration, National Aeronautics and Space Administration, and the United States Air Force, U.S. Government Printing Office, Washington, DC, 1976
2. B. A. Banks , K. K.de Groh, S.Rutledge and F. J.DiFilippo, Prediction of In-Space Durability of Protected Polymers Based on Ground Laboratory Thermal Energy Atomic Oxygen, NASA TM-107209, NationalAeronautics and Space Administration, Washington, DC, 1996
3. D. Dooling and M. M.Finckenor, Material Selection Guidelines to Limit Atomic Oxygen Effects on Spacecraft Surfaces, NASA/TP-1999–209260, National Aeronautics and Space Administration, Washington, D.C, 1999
4. T. K. Minton and D. J.Garton, Dynamics of Atomic-Oxygen-Induced Polymer Degradation in Low-Earth Orbit, in Advanced Series in Physical Chemistry11: Chemical Dynamics in Extreme Environments, ed. Dressler R. A., World Scientific, Singapore, 2001, p. 420
5. B. A. Banks , K. K.de Groh, S. K.Miller, Low Earth Orbital Atomic Oxygen Interactions with Spacecraft Materials, NASA/TM-2004-213400, National Aeronautics and Space Administration, Washington, D.C., 2004