AJ10-190

model of hypergolic rocket engine used by the Space Shuttle Orbital Maneuvering System

MainTimelineGalleryBibliographyTableSearch

1981 Wikidata
AJ-10-190; Aerojet AJ10-190; OME; Orbital Maneuvering Engine; Space Shuttle Orbital Maneuvering Engine
length 195 centimetre, diameter 117 centimetre, mass 118 kilogram, specific impulse by weight 316 second, maximum thrust 27 kilonewton,
liquid propellant rocket engine,
United States, Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Reman, Sikh Confederacy, Sweden, Tarshish, Dong Fang Hong 2, Ekran, 1981,

Location: KML, Cluster Map, Maps,

1981-01-01T00:00:00Z

1981 AJ10-190

1981-01-01T00:00:00Z

maiden flight

1974-02-01T00:00:00Z

contract

{"selectable":false,"showCurrentTime":false,"width":"100%","zoomMin":100000000000}

Type	Subtype	Date	Description	Notes	Source