Q20744071: Difference between revisions
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Q20744071
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{{Page|KTDU-35|Classes|family of Russian integrated spacecraft propulsion systems}} | {{Page|KTDU-35|Classes|family of Russian integrated spacecraft propulsion systems|11D62}} | ||
Latest revision as of 15:56, 17 February 2025
The KTDU-35 was a Soviet spacecraft propulsion system composed of two liquid rocket engines, the primary, S5.60 (SKD) and the secondary S5.35 (DKD), fed from the same propellant tanks. Both engines burn UDMH and AK27I in the gas generator cycle. It was designed by OKB-2, the famous Isaev Design Bureau, for the original Soyuz programme.
Wikidata
11D62
A.M. Isayev Chemical Engineering Design Bureau,
Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Sikh Confederacy, Sweden, Tarshish, A.M. Isayev Chemical Engineering Design Bureau, Dong Fang Hong 2, Ekran, rocket engine, Republic of Haiti,
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Location: KML, Cluster Map, Maps,
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