Talk:RS-27A

Number of chambers
The current version of the article states the number of chambers as 2. Surely not? (sdsds - talk) 02:23, 25 September 2009 (UTC)

Correct. It's a single chamber engine. 148.76.41.216 (talk) 23:47, 26 June 2021 (UTC)

Merging RS-27 and RS-27A?
The articles qualify at best as stubs, and are really short. I guess it would have been rather more logical to consolidate them on a single article. May be even with he H-1?

That would be logical 148.76.41.216 (talk) 23:46, 26 June 2021 (UTC)

I plan on merging these articles (RS-27 & RS-27A) in the coming days unless someone objects. They're both stubs and the -A variant is just that, a variant.(talk) 07:02:25 1 June 2024 (UTC)

Amount of Thrust
AFAIK, the RS-27A engine generated 240,000 pounds of thrust at Sea Level. In the Specs Box, it says 200,000. 148.76.41.216 (talk) 23:49, 26 June 2021 (UTC)