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Lessons Learned - Galileo Retro Propulsion Module and Pyro Power System Interaction

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:04:46Z
date available2017-09-04T16:04:46Z
date copyright34690
date issued1994
identifier otherRUAEQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/67974
description abstractAbstract:
Galileo design optimizations over the years exacerbated interactions between spacecraft power and the propellant tanks. During the cruise phase, high power and heat dissipation near the propellant tanks combined with an enhanced tank load to increase the tank pressure.
A thorough analysis should be conducted before changes are made to one or more of the flight project elements that occur late in the development cycle or well into the test program.
languageEnglish
titleNASA-LLIS-0364num
titleLessons Learned - Galileo Retro Propulsion Module and Pyro Power System Interactionen
typestandard
page3
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1994
contenttypefulltext
subject keywordsConfiguration Management
subject keywordsTest & Verification


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