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Lessons Learned – Galileo Retro Propulsion Module (RPM) Flow Decay Problem

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:11:22Z
date available2017-09-04T16:11:22Z
date copyright09/01/1993
date issued1993
identifier otherSMAEQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/74600
description abstractAbstract:
To reduce costs, the Mars Observer propulsion and other subsystems followed design practices more common to earth-orbiting satellites than to planetary missions. Consider contractor experience in bipropellant spacecraft propulsion system design in source selection. To manage risk on one-of-akind developments, assure thorough technical oversight of contractors with limited experience in the design of interplanetary spacecraft.
languageEnglish
titleNASA-LLIS-0305num
titleLessons Learned – Galileo Retro Propulsion Module (RPM) Flow Decay Problemen
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1993
contenttypefulltext
subject keywordsParts Materials & Processes
subject keywordsSpacecraft


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