Q5310218: Difference between revisions
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{{Page|dual-mode propulsion system|Classes|spacecraft propulsion system which uses different propellants for different phases of flight}} | {{Page|dual-mode propulsion system|Classes|spacecraft propulsion system which uses different propellants for different phases of flight|dual-mode propulsion rocket}} | ||
Latest revision as of 16:02, 17 February 2025
Dual mode propulsion systems combine the high efficiency of bipropellant rockets with the reliability and simplicity of monopropellant rockets.
Wikidata
dual-mode propulsion rocket
Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Reman, Sikh Confederacy, Sweden, Tarshish, Dong Fang Hong 2, Ekran, rocket engine, Republic of Haiti,
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Location: KML, Cluster Map, Maps,
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