Show simple item record

Lessons Learned - RCS Thruster Heater Power During Ferry Flight Stopovers; RCS Thruster Ferry Plug Removal; Hypergol Exhaust System Indicator Lamp

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:45:15Z
date available2017-09-04T18:45:15Z
date copyright02/12/1992
date issued1992
identifier otherKGYCQCAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsessionid=3826AF679D40527318548F1EFDEC014A/handle/yse/226730
description abstractDescription of Driving Event:
During the removal of the flight reaction control system (RCS) ferry plugs from the orbiter, between 1/4 and 3/4 cup of monomethylhydrazine (MMH) fuel spilled from the thruster. The liquid contacted the gloves and right shoe of the technician pulling the plug. The RCS thruster valve seals have a history of sensitivity to temperatures below 60 deg F. To limit the potential for leakage, the RCS thruster heater power unit should remain on throughout the Dryden Flight Research Facility (DFRF) safing and ferry period, including flight stopovers and KSC offload.
languageEnglish
titleNASA-LLIS-0059num
titleLessons Learned - RCS Thruster Heater Power During Ferry Flight Stopovers; RCS Thruster Ferry Plug Removal; Hypergol Exhaust System Indicator Lampen
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1992
contenttypefulltext
subject keywordsEnergetic Materials - Explosive/Propellant/Pyrotechnic
subject keywordsFlight Equipment
subject keywordsFlight Operations
subject keywordsGround Equipment
subject keywordsGround Operations
subject keywordsHardware
subject keywordsHazardous/Toxic Waste/Materials
subject keywordsLaunch Vehicle
subject keywordsSafety & Mission Assurance


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record