HM7A

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Q97216614




European rocket engine

1979  Wikidata
HM-7A; HM7-A
diameter 0.93 metre, mass 149 kilogram, height 1.71 metre, specific impulse by weight 443 second, specific impulse by weight 308 second, maximum thrust 42.9 kilonewton, maximum thrust 61.7 kilonewton, 
cryogenic rocket engine, Safran Aircraft Engines, France, 
Ashkenaz, Calvinist Republic of Ghent, Chinland, France, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Sikh Confederacy, Tarshish, cryogenic rocket engine, Dong Fang Hong 2, Ekran, 1979, Republic of Haiti, 1970s, 

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Location: KML, Cluster Map, Maps,

    1979-12-24T00:00:00Z
    1979-12-24T00:00:00Z
    1979 HM7A
    1979-12-24T00:00:00Z
    1979-12-24T00:00:00Z
    maiden flight
    1973-01-01T00:00:00Z
    1973-01-01T00:00:00Z
    new product development
    1986-02-22T00:00:00Z
    1986-02-22T00:00:00Z
    last flight
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