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U.S. Department of Energy
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PRINCIPLES FOR THE CALCULATION OF RADIATION DOSE RATES IN SPACE VEHICLES. Report No. 63270-05-01

Technical Report ·
OSTI ID:4838164
An analysis is presented which takes into account the angular distribution of the incident protons and electrons and the angular distribution of the electron bremsstrahlung. The distribution with depth in the propellant is determined for the dose rate due to protons, for the dose rate due to electron bremsstrahlung, and for the deposition of stopped protons. Whereas the dose rates for monoenergetic protons or electrons are maximum at the surface of the propellant, the deposition of protons has its minimum at the surface and increases linearly with depth up to the range of the protons. For the case of protons, the maximum surface dose rate depends primarily on the total number of protons striking the surface, and only slightly on their energy, so long as their energy is sufficient for them to clearly penetrate the surface medium. Illustrative calculations ai-e carried out for the Freden and White spectrum of protons and for the Walt et al., spectrum of electrons incident on thin-walled stainless steel vehicles carrying liquid H/sub 2/ or liquid O/sub 2/. The numerical results for O/sub 2/ would be closely similar to those for biological materials. (auth)
Research Organization:
Massachusetts Inst. of Tech., Cambridge
NSA Number:
NSA-16-021844
OSTI ID:
4838164
Report Number(s):
AD-263476
Country of Publication:
United States
Language:
English