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Lessons Learned – Performance Decrease due to Propulsion Thruster Plume Impingement on the Voyager Spacecraft

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:46:07Z
date available2017-09-04T17:46:07Z
date copyright01/31/1995
date issued1995
identifier otherELBEQCAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/169300
description abstractAbstract:
A 21{}hortfall in Voyager's velocity change was suspected to be due to exhaust plume impingement. Due to the complexity of spacecraft/thruster configurations, additional care must be taken in the development and utilization of spacecraft and plume models. Analysis should be conducted on early and final designs.
languageEnglish
titleNASA-LLIS-0377num
titleLessons Learned – Performance Decrease due to Propulsion Thruster Plume Impingement on the Voyager Spacecraften
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1995
contenttypefulltext
subject keywordsFlight Equipment
subject keywordsSpacecraft


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