NASA-LLIS-0792

Lessons Learned – Radiation Design Margin Requirement

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T17:16:55Z
date available	2017-09-04T17:16:55Z
date copyright	04/17/2000
date issued	2000
identifier other	ZHDEQCAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std/handle/yse/140360
description abstract	Practice: Design spacecraft hardware assemblies with the required radiation design margin (RDM) to assure that they can withstand ionization effects and displacement damage resulting from the flight radiation environment. The term "margin" does not imply a known factor of safety but rather accommodates the uncertainty in the radiation susceptibility predictions. The reliability requirement to survive for a period of time in the anticipated mission radiation environment is a spacecraft design driver.
language	English
title	NASA-LLIS-0792	num
title	Lessons Learned – Radiation Design Margin Requirement	en
type	standard
page	8
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;2000
contenttype	fulltext