Development and application of a 3-D geometry/mass model for LDEF satellite ionizing radiation assessments

B. L. Colborn; T. W. Armstrong

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NASA NTRS · 19920017993

Development and application of a 3-D geometry/mass model for LDEF satellite ionizing radiation assessments

B. L. Colborn·T. W. Armstrong

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Abstract

A computer model of the three dimensional geometry and material distributions for the LDEF spacecraft, experiment trays, and, for selected trays, the components of experiments within a tray was developed for use in ionizing radiation assessments. The model is being applied to provide 3-D shielding distributions around radiation dosimeters to aid in data interpretation, particularly in assessing the directional properties of the radiation exposure. Also, the model has been interfaced with radiation transport codes for 3-D dosimetry response predictions and for calculations related to determining the accuracy of trapped proton and cosmic ray environment models. The methodology is described used in developing the 3-D LDEF model and the level of detail incorporated. Currently, the trays modeled in detail are F2, F8, and H12 and H3. Applications of the model which are discussed include the 3-D shielding distributions around various dosimeters, the influence of shielding on dosimetry responses, and comparisons of dose predictions based on the present 3-D model vs those from 1-D geometry model approximations used in initial estimates.

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B. L. Colborn, T. W. Armstrong. 1992-06-01. Development and application of a 3-D geometry/mass model for LDEF satellite ionizing radiation assessments. https://ntrs.nasa.gov/citations/19920017993

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