HM7A

European rocket engine

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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,
France, cryogenic rocket engine, Dong Fang Hong 2, 1979, 1970s,

Location: KML, Cluster Map, Maps,

1979-12-24T00:00:00Z

1979 HM7A

1979-12-24T00:00:00Z

maiden flight

1973-01-01T00:00:00Z

new product development

1986-02-22T00:00:00Z

last flight

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Type	Subtype	Date	Description	Notes	Source