Q7387063: Difference between revisions
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{{Page|S-III|Classes|proposed rocket stage for the Saturn C}} | {{Page|S-III|Classes|proposed rocket stage for the Saturn C|Saturn S-III}} | ||
Latest revision as of 14:02, 17 February 2025
The S-III was a proposed third stage of the early Saturn C designs for a five-stage Saturn launch vehicle. The Saturn C configurations were based on a "building block" approach, in which the upper stages would be test-flown before the intermediate stages. The S-III was to have been fueled with liquid oxygen and liquid hydrogen and powered by two J-2 engines. The original Saturn C-2 design would have been a three- or four-stage launch vehicle using the S-I plus S-III plus S-IV stages plus, for some missions, S-V.
Wikidata
Saturn S-III
United States,
United States, Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Sikh Confederacy, Tarshish, Dong Fang Hong 2, Ekran, Republic of Haiti,
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Location: KML, Cluster Map, Maps,
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