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Early Results from the Advanced Radiation Protection Thick GCR Shielding ProjectThe Advanced Radiation Protection Thick Galactic Cosmic Ray (GCR) Shielding Project leverages experimental and modeling approaches to validate a predicted minimum in the radiation exposure versus shielding depth curve. Preliminary results of space radiation models indicate that a minimum in the dose equivalent versus aluminum shielding thickness may exist in the 20-30 g/cm2 region. For greater shield thickness, dose equivalent increases due to secondary neutron and light particle production. This result goes against the long held belief in the space radiation shielding community that increasing shielding thickness will decrease risk to crew health. A comprehensive modeling effort was undertaken to verify the preliminary modeling results using multiple Monte Carlo and deterministic space radiation transport codes. These results verified the preliminary findings of a minimum and helped drive the design of the experimental component of the project. In first-of-their-kind experiments performed at the NASA Space Radiation Laboratory, neutrons and light ions were measured between large thicknesses of aluminum shielding. Both an upstream and a downstream shield were incorporated into the experiment to represent the radiation environment inside a spacecraft. These measurements are used to validate the Monte Carlo codes and derive uncertainty distributions for exposure estimates behind thick shielding similar to that provided by spacecraft on a Mars mission. Preliminary results for all aspects of the project will be presented.
Document ID
20170005580
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Norman, Ryan B.
(NASA Langley Research Center Hampton, VA, United States)
Clowdsley, Martha
(NASA Langley Research Center Hampton, VA, United States)
Slaba, Tony
(NASA Langley Research Center Hampton, VA, United States)
Heilbronn, Lawrence
(Tennessee Univ. Knoxville, TN, United States)
Zeitlin, Cary
(Leidos, Inc. Houston, TX, United States)
Kenny, Sean
(NASA Langley Research Center Hampton, VA, United States)
Crespo, Luis
(NASA Langley Research Center Hampton, VA, United States)
Giesy, Daniel
(NASA Langley Research Center Hampton, VA, United States)
Warner, James
(NASA Langley Research Center Hampton, VA, United States)
McGirl, Natalie
(Tennessee Univ. Knoxville, TN, United States)
Castellanos, Luis
(Tennessee Univ. Knoxville, TN, United States)
Srikrishna, Ashwin
(Tennessee Univ. Knoxville, TN, United States)
Beach, Matthew
(National Inst. of Aerospace Hampton, VA, United States)
Bahadori, Amir
(Kansas State Univ. Manhattan, KS, United States)
Reddell, Brandon
(NASA Johnson Space Center Houston, TX, United States)
Singleterry, Robert
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
June 14, 2017
Publication Date
May 15, 2017
Subject Category
Space Radiation
Spacecraft Design, Testing And Performance
Report/Patent Number
NF1676L-27179
Meeting Information
Meeting: Applied Space Environments Conference (ASEC) 2017
Location: Huntsville, AL
Country: United States
Start Date: May 15, 2017
End Date: May 19, 2017
Sponsors: Universities Space Research Association
Funding Number(s)
WBS: WBS 651549.02.07.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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