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Radiation Dosages From Electrons and Bremsstrahlung in the Van Allen BeltsRadiation dose rates have been calculated for six electron spectra. The decrease in dose rate with shielding was determined -- and in each case the electron does becomes insignificant with 2 to 6 gm/cm2 of aluminum. Electron bremsstrahlung doe rates versus absorber thickness were also calculated. Detailed dosage calculations for an Apollo-type spacecraft were made and mission dosages for four lunar trajectories are given, to show the effects of trajectory selection. These are compared with the dosages from protons and secondary neutrons in the Van Allen Belt. Doses as a function of orbital altitude, of inclination and of absorber thickness are also presented for the latest version of the inner belt.
Document ID
19630005277
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
S L Russak
(The Martin Company Baltimore, MD, United States)
Date Acquired
August 1, 2013
Publication Date
November 7, 1962
Publication Information
Publication: Proceedings of the Symposium on the Protection Against Radiation Hazards in Space
Publisher: United States Atomic Energy Commission
Volume: 1
Issue: 1 & 2
Issue Publication Date: November 5, 1962
Subject Category
Structural Mechanics
Report/Patent Number
63N15153
TID-7652
Meeting Information
Meeting: Protection Against Radiation Hazards in Space
Location: Gatlinburg, TN
Country: US
Start Date: November 5, 1962
End Date: November 7, 1962
Sponsors: Oak Ridge National Laboratory, American Nuclear Society, National Aeronautics and Space Administration
Accession Number
63N15153
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Keywords
SPACECRAFT SHIELDING
VAN ALLEN BELT
ELECTRON
RADIATION HAZARD
BREMSSTRAHLUNG
RADIATION DOSE
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