On the validity of the aluminum equivalent approximation in space radiation shielding applications-Reference-Cited by-同舟云学术

On the validity of the aluminum equivalent approximation in space radiation shielding applications

Published:2010-09 Issue:6 Volume:46 Page:719-727
ISSN:0273-1177
Container-title:Advances in Space Research
language:en
Short-container-title:Advances in Space Research

Author:

Badavi Francis F.,Adams Daniel O.,Wilson John W.

Publisher

Elsevier BV

Subject

Space and Planetary Science,Aerospace Engineering,General Earth and Planetary Sciences,Atmospheric Science,Geophysics,Astronomy and Astrophysics

Reference18 articles.

1. Adams, D.O., Webb, N.J., Yarger, C.B., Hunter, A., Oborn, K.D. Multi-functional sandwich composites for spacecraft applications: an initial assessment. NASA-CR- 2007-214880, 2007.

2. Armstrong, T.W., Colborn, B.L., Ringler, S.J. Radiation dose estimation to the crew inside the International Space Station Lab, Hab, node 1, node 2, and airlock modules. SAIC-TN-9601, 1996.

3. Properties of high energy beams from a 600MeV synchrocyclotron;Baarli,1967

4. Badavi, F.F., West, K.J., Nealy, J.E., Wilson, J.W., Abrahms, B.L., Luetke, N.J. A dynamic/anisotropic Low Earth Orbit (LEO) ionizing radiation model. NASA-TP- 2006-214533, 2006.

5. Badavi, F.F., Stewart-Sloan, C.R., Adams, D.O., Wilson, J.W. Radiation protection effectiveness of polymeric based shielding materials at Low Earth Orbit. SAMPE paper 2008-L002, 2008.

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