Radiation dose and shielding for the Space Station.
Significant differences in dose prediction for Space Station arise depending on whether or not the magnetic field model is extrapolated into the future.   The basis for these calculations is examined in detail, and the importance of the residual atmospheric layer at altitudes below 1000 km, with respect to radiation attenuation is emphasized.  Dosimetry results from Shuttle flights are presented and compared with the computed results.  It is recommended that, at this stage, no extrapolation of the magnetic field into the future be included in the calculations.  A model adjustment, to replace this arbitrary procedure is presented.  Dose predictions indicate that, at altitudes below 500 km and at low inclination, and with nominal module wall thickness (0.125 in. aluminum), orbit stay times of 90 days in Space Station would result in quarterly radiation doses to the crew, which are well within present limits both for males and females.  Countermeasures would be required for stay times of a year or more and the measure of increasing shielding is examined.
McCormack
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PD
National Aeronautics and Space Administration, Office of Space Station, Washington, DC 20546.
D000535:Aluminum; D003198:Computer Simulation; D003359:Cosmic Radiation / Q000009:adverse effects*; D018478:Extravehicular Activity; D005260:Female; D005676:Gravity Suits; D006801:Humans; D008280:Magnetics; D008297:Male; D008962:Models, Theoretical; D011829:Radiation Dosage; D011834:Radiation Monitoring; D011835:Radiation Protection / Q000379:methods* / Q000592:standards; D016082:Solar System; D013026:Space Flight; D018531:Spacecraft / Q000295:instrumentation*
D000535:Aluminum