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Should this article be combined with the rest of the Soyuz 2.1a/b/ST article? It’s still in that family, sharing launch facilities, tooling and design features. Is there a compelling reason to keep it separate?Blastr42 (talk)01:33, 10 December 2017 (UTC)[reply]
No, this rocket is too different. It's a repurposed Soyuz center core, with a different engine and structural reinforcements. Our article calls it a "heavily modified derivative". Naming is alas misleading; wish they had kept the "Soyuz-1" development name. —JFGtalk01:10, 11 December 2017 (UTC)[reply]
The following is a closed discussion of arequested move.Please do not modify it. Subsequent comments should be made in a new section on the talk page. Editors desiring to contest the closing decision should consider amove review after discussing it on the closer's talk page. No further edits should be made to this discussion.
@Hellbus: The citing in the article might use a dot, but many of the references were changed from dashes to dots inthis edit byUser:CRS-20 in August 2020.
Clicking on the references show that the majority of them do use "Soyuz-2-1v", see:[1],[2] or[3] as examples.Also, the manufacturer's website uses the dash form, see source:[4].Happily888 (talk)04:32, 18 October 2022 (UTC); edited 04:49, 18 October 2022 (UTC)[reply]
The discussion above is closed.Please do not modify it. Subsequent comments should be made on the appropriate discussion page. No further edits should be made to this discussion.