Practical response to radiation assessment for spacecraft designAn innovative radiative assessment system that combines the advantages of computer-aided design and enhanced radiative transport codes is described. An analysis of a Space Station habitat module is carried out. A scheme that makes it possible to account for anisotropies existing in the radiation environment of LEO is developed.
Document ID
19910034671
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Appleby, M. H. (Boeing Co. Huntsville, AL, United States)
Tanner, E. R., II (Boeing Co. Huntsville, AL, United States)
Nealy, J. E. (NASA Langley Research Center Hampton, VA, United States)
Ryder, S. P. (Boeing Co. Huntsville, AL, United States)
Pike, E. L. (Intergraph Corp. Huntsville, AL, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 91-0425Report Number: AIAA PAPER 91-0425