A comparison of radiation shielding effectiveness of materials for highly elliptical orbits |
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Authors: | A. Emmanuel J. Raghavan R. Harris P. Ferguson |
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Affiliation: | 1. Composite Materials & Structures Research Group, Mechanical Engineering Department, University of Manitoba, Winnipeg, MB R3T 6A6, Canada;2. Magellan Aerospace, Winnipeg, MB R3C 2S4, Canada |
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Abstract: | The Canadian Space Agency (CSA) has proposed a Polar Communications and Weather (PCW) satellite mission, in conjunction with other partners. The PCW will provide essential communications and meteorological services to the Canadian Arctic, as well as space weather observations of in situ ionizing radiation along the orbit. The CSA has identified three potential Highly Elliptical Orbits (HEOs) for a PCW satellite constellation, Molniya, Modified Tundra and Triple Apogee (TAP), each having specific merits, which would directly benefit the performance/longevity of a PCW spacecraft. Radiation shielding effectiveness of various materials was studied for the three PCW orbit options to determine the feasibility of employing materials other than conventional aluminium to achieve a specified spacecraft shielding level with weight savings over aluminium. It was found that, depending on the orbit-specific radiation environment characteristics, the benefits of using polyethylene based materials is significant enough (e.g., 22% in Molniya for PE at 50 krad TID) to merit further investigation. |
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Keywords: | Radiation shielding Simulation Highly elliptical orbit Satellite Shielding material |
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