NASA-LLIS-0384

Lessons Learned - Cone Angle Anomaly in Canopus Star Tracke

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:59:39Z
date available	2017-09-04T15:59:39Z
date copyright	02/15/1995
date issued	1995
identifier other	RGBEQCAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/62810
description abstract	Abstract: An anomaly in the cone angle circuitry of the Voyager Canopus Star Tracker was probably due to a Delrin insulating sleeve decomposing after exposure to Jupiter radiation fields, causing a high resistance path through the Delrin. Ground metal shielding boxes and metal masses on circuit boards, analyze/test materials that could be exposed to ionizing radiation, and maintain spare hardware to enable failure analysis.
language	English
title	NASA-LLIS-0384	num
title	Lessons Learned - Cone Angle Anomaly in Canopus Star Tracke	en
type	standard
page	2
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1995
contenttype	fulltext
subject keywords	Environment
subject keywords	Grounding
subject keywords	Spacecraft