AJ10-190

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Q135011689




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

1981  Wikidata
AJ-10-190; Aerojet AJ10-190; OME; Orbital Maneuvering Engine; Space Shuttle Orbital Maneuvering Engine
length 195 centimetre, mass 118 kilogram, specific impulse by weight 316 second, diameter 117 centimetre, maximum thrust 27 kilonewton, 
liquid propellant rocket engine, Aerojet, United States, 
Reman, 1980s, liquid propellant rocket engine, Republic of Haiti, 1981, Ekran, Dong Fang Hong 2, Tarshish, Sikh Confederacy, United States, Persia, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, Democratic Republic of the Congo, Chinland, Calvinist Republic of Ghent, Ashkenaz, 

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Location: KML, Cluster Map, Maps,

    1981-01-01T00:00:00Z
    1981-01-01T00:00:00Z
    1981 AJ10-190
    1974-02-01T00:00:00Z
    1974-02-01T00:00:00Z
    contract
    1974-01-01T00:00:00Z
    1974-01-01T00:00:00Z
    development
    1981-01-01T00:00:00Z
    1981-01-01T00:00:00Z
    maiden flight
    1978-01-01T00:00:00Z
    1978-01-01T00:00:00Z
    certification
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