Space Shuttle Orbital Maneuvering System

GPTKB entity

Predicate	Object
gptkbp:instanceOf	gptkb:rocket_engine_system
gptkbp:abbreviation	gptkb:OMS
gptkbp:burnTime	up to 1,000 seconds per mission
gptkbp:countryOfOrigin	gptkb:United_States
gptkbp:engineType	pressure-fed
gptkbp:firstFlight	gptkb:STS-1
gptkbp:gimbaled	no
gptkbp:lastFlight	gptkb:STS-135
gptkbp:location	aft fuselage of Space Shuttle orbiter
gptkbp:manufacturer	gptkb:Rockwell_International
gptkbp:numberOfEngines	2
gptkbp:partOf	gptkb:Space_Shuttle
gptkbp:propulsion	monomethylhydrazine nitrogen tetroxide
gptkbp:relatedTo	gptkb:Space_Shuttle_Main_Engine gptkb:Reaction_Control_System
gptkbp:restartable	yes
gptkbp:status	retired
gptkbp:thrust	26.7 kN
gptkbp:usedFor	deorbit burns orbital maneuvers orbit insertion orbit circularization
gptkbp:usedOn	gptkb:Columbia gptkb:Endeavour gptkb:Challenger gptkb:Atlantis gptkb:Discovery
gptkbp:bfsParent	gptkb:AJ10 gptkb:AJ10-118K gptkb:Aerojet_Rocketdyne_AJ10
gptkbp:bfsLayer	8
https://www.w3.org/2000/01/rdf-schema#label	Space Shuttle Orbital Maneuvering System