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NASA-LLIS-0424

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

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1996

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.
URI: http://yse.yabesh.ir/std;jsessionid=3826AF679D40527318548F1EFDEC014A/handle/yse/228258
Subject: Hardware
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    NASA-LLIS-0424

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:47:04Z
date available2017-09-04T18:47:04Z
date copyright07/10/1996
date issued1996
identifier otherKLBEQCAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsessionid=3826AF679D40527318548F1EFDEC014A/handle/yse/228258
description abstractAbstract:
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.
languageEnglish
titleNASA-LLIS-0424num
titleLessons Learned – Voyager Unbalanced Attitude Control System and Thruster Impingement Effects on Navigation (~1977)en
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1996
contenttypefulltext
subject keywordsHardware
subject keywordsSpacecraft
subject keywordsTrajectory Accuracy
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