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0.l8-mil aluminum Aeronautics and Space aluminum foil analysis employs numerical applied to three approximating the energy Armstrong atomic density atomic number average path length CALCULATION OF ELECTRON Characteristic variations D-2010 National Aeronautics dE/dx deposited energy deposited in shielded DEPOSITION IN THIN-FILM determine the average Echo II balloon ELECTRON ENERGY DEPOSITION electron kinetic energy electron with incident electrons entering employs numerical methods Energy absorbed energy loss energy with incident entering the material equation exit energy films by electrons function of incident incident electron kinetic incident energy incident kinetic energy inflated Echo Langley Research Center length to range material normal mean excitation potential methods to determine NASA NASA TN NASA TECHNICAL NOTE OTS price parabolas polymer films potential are known presented for approximating procedure rises slowly thereafter second Mylar layer shielded and unshielded shielded mate Space Administration surface TECHNICAL NOTE D-2010 Teichman and Ernest THIN-FILM POLYMERIC MATERIALS trons unshielded poly unshielded polypropylene