NASA-LLIS-0768

Lessons Learned – Thermal Design Practices for Electronic Assemblies

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T18:21:09Z
date available	2017-09-04T18:21:09Z
date copyright	04/06/2000
date issued	2000
identifier other	HYCEQCAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/203635
description abstract	Practice: Insure that thermal design practices for electronic assemblies will meet the requirements of the combined ground and flight environmental conditions defined by the spacecraft mission. Special emphasis should be placed on limiting the junction temperature of all active components. Proper thermal design practices take into consideration the need for ease of operation and repairability to enhance overall system reliability. The environmental conditions that the spacecraft encounters, both on the ground and in flight, are designed to include adequate margin. The use of proper thermal design practices ensures that the assemblies will survive the expected environmental conditions.
language	English
title	NASA-LLIS-0768	num
title	Lessons Learned – Thermal Design Practices for Electronic Assemblies	en
type	standard
page	3
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;2000
contenttype	fulltext