Show simple item record

NASA-LLIS-0961

Lessons Learned – Space Shuttle Main Engine (SSME) Component Test Facility: Simplicity of Design

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:43:32Z
date available2017-09-04T17:43:32Z
date copyright05/15/1995
date issued1995
identifier otherEDUEQCAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/166592
description abstractDescription of Driving Event:
The SSME turbobpump test stand had approximately 2,000 valves, two dozen, which were servooperated. Facility preburner valves weighed as much as 5 tons for the 14,000 psi system. Facility problems were abundant. In one test, for example, a facility rotary flowmeter failed, releasing flowmeter blades into the LOX flow stream, causing a fire. A similar failure also occurred on a fuel facility subsystem.
languageEnglish
titleNASA-LLIS-0961num
titleLessons Learned – Space Shuttle Main Engine (SSME) Component Test Facility: Simplicity of Designen
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


Files in this item

Thumbnail
Name:
EDUEQCAAAAAAAAAA.pdf
Size:
13.21Kb
Format:
PDF
View/Open

This item appears in the following Collection(s)

Show simple item record