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Shielding Requirements for Manned Orbiting Space StationsA detailed parametric investigation of radiation shielding requirements was performed for first generation manned orbiting space stations. Two specific space station designs were studied; the results of the shielding analysis are based on the actual geometry of the vehicles, onboard equipment, and supplies. Results are presented for circular orbits ranging from 100 to 600 nautical miles and from 29° to 90° inclination. The effects of the geometry of the space stations, the use of personal shielding, and the use of particular shielding materials are discussed.
Document ID
19650025020
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
T. M. Jordan
( Douglas Aircraft Co., Inc. Santa Monica, CA, United States)
E. F. Koprowski
(Douglas Aircraft Co., Inc. Santa Monica, CA, United States)
R. W. Langley
(Douglas Aircraft Co., Inc. Santa Monica, CA, United States)
Date Acquired
August 2, 2013
Publication Date
January 1, 1965
Publication Information
Publication: Second Symposium on Protection Against Radiations in Space
Publisher: National Aeronautics and Space Administration
Subject Category
Space Vehicles
Report/Patent Number
N65-34621
Meeting Information
Meeting: Second Symposium on Protection Against Radiations in Space
Location: Gatlinburg, TN
Country: US
Start Date: October 12, 1964
End Date: October 14, 1964
Sponsors: National Aeronautics and Space Administration
Accession Number
65N34621
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
MANNED ORBITAL SPACE STATION /MOSS/
RADIATION SHIELDING
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