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NASA-LLIS-0960

Lessons Learned – Space Shuttle Main Engine (SSME): Integrated Subsystem Test Bed

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:51:34Z
date available2017-09-04T15:51:34Z
date copyright05/15/1995
date issued1995
identifier otherBDUEQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/54723
description abstractDescription of Driving Event:
The SSME components were originally planned to be tested on a "bobtail" engine. To provide integrated testing, which takes into account the component interactions, however it was decided to add a shortened version of the thrust chamber. The shortened version had an area ratio of 35:1 versus the flight configuration requirements of 77.5 to 1. The test engine could throttle to 50% without requiring a vacuum chamber.
languageEnglish
titleNASA-LLIS-0960num
titleLessons Learned – Space Shuttle Main Engine (SSME): Integrated Subsystem Test Beden
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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