NASA-LLIS-0424

Lessons Learned – Voyager Unbalanced Attitude Control System and Thruster Impingement Effects on Navigation (~1977)

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T18:47:04Z
date available	2017-09-04T18:47:04Z
date copyright	07/10/1996
date issued	1996
identifier other	KLBEQCAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;query=autho162/handle/yse/228258
description abstract	Abstract: Shortly after the launch of Voyager, unexpected dynamic effects necessitated additional orbit determination analysis, testing, and modeling to ensure an accurate trajectory. Perform careful coordinated pre-flight analysis to determine the impact of such effects as torques induced by solar pressure and gas impingement on the spacecraft structure. Design and test to avoid impingement problems.
language	English
title	NASA-LLIS-0424	num
title	Lessons Learned – Voyager Unbalanced Attitude Control System and Thruster Impingement Effects on Navigation (~1977)	en
type	standard
page	2
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1996
contenttype	fulltext
subject keywords	Hardware
subject keywords	Spacecraft
subject keywords	Trajectory Accuracy