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Lessons Learned - Galileo Messerschmitt-Bolkow-Blohm (MBB) Ten Newton Hot Start Phenomena

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:19:03Z
date available2017-09-04T18:19:03Z
date copyright34652
date issued1994
identifier otherHTAEQCAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/201743
description abstractAbstract:
During confidence testing of the MBB Galileo Ten Newton (N) Engine at MBB in November 1988, rapid increases in combustion chamber temperature ("hot starts") were sometimes observed immediately after ignition of the engine. Examination of test data from the previous flight engine acceptance tests showed evidence of hot starts, but JPL had not witnessed these earlier tests.
The lesson recommends several measures to assure that rocket engine development and qualification test instrumentation and test documentation are sufficient to detect and diagnose combustion instabilities.
languageEnglish
titleNASA-LLIS-0351num
titleLessons Learned - Galileo Messerschmitt-Bolkow-Blohm (MBB) Ten Newton Hot Start Phenomenaen
typestandard
page3
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1994
contenttypefulltext
subject keywordsEnergetic Materials - Explosive/Propellant/Pyrotechnic
subject keywordsResearch & Development
subject keywordsSupplier Testing
subject keywordsTest & Verification


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