Q131142596: Difference between revisions

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Q131142596
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Latest revision as of 15:52, 17 February 2025




bi-propellant thruster engine used on spacecraft

Wikidata
Gravitics GM100
mass 4.5 kilogram, maximum thrust 445 newton, specific impulse by weight 310 second, 
rocket engine, thruster, GraviticsUnited States
United StatesAshkenazCalvinist Republic of GhentChinlandHavilahKingdom of Martabam-hongsawatoiKingdom of WolaitaPersiaSikh ConfederacyTarshishDong Fang Hong 2Ekranrocket engineRepublic of HaitiGravitics


Location: KML, Cluster Map, Maps,


      TypeSubtypeDateDescriptionNotesSource