Q97216614: Difference between revisions
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Q97216614
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Latest revision as of 12:46, 2 September 2025
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,
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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