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NASA-LLIS-0967

Lessons Learned - Space Shuttle Main Engine (SSME): Instrumented Safety Checks During Engine Startup

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1995

Abstract: Description of Driving Event:
Turbine speed must be high enough at the time of main combustion chamber priming to be able to pump hydrogen through the downstream system against the back pressure rise created by the chamber priming, or an engine burnout will occur due to the oxygen rich combustion.
URI: https://yse.yabesh.ir/std/handle/yse/21616
Subject: Configuration Management
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  • NASA - National Aeronautics and Space Administration (NASA)
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    NASA-LLIS-0967

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:21:38Z
date available2017-09-04T15:21:38Z
date copyright05/15/1995
date issued1995
identifier otherMZTEQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/21616
description abstractDescription of Driving Event:
Turbine speed must be high enough at the time of main combustion chamber priming to be able to pump hydrogen through the downstream system against the back pressure rise created by the chamber priming, or an engine burnout will occur due to the oxygen rich combustion.
languageEnglish
titleNASA-LLIS-0967num
titleLessons Learned - Space Shuttle Main Engine (SSME): Instrumented Safety Checks During Engine Startupen
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1995
contenttypefulltext
subject keywordsConfiguration Management
subject keywordsCryogenic Systems
subject keywordsGround Equipment
subject keywordsHardware
subject keywordsLaunch Vehicle
subject keywordsParts Materials & Processes
subject keywordsSafety & Mission Assurance
subject keywordsSpacecraft
subject keywordsTest Article
subject keywordsTest Facility
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