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Talk:Executor (rocket engine)

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This is an old revision of this page, as edited by Blazotron (talk | contribs) at 07:38, 9 April 2012 (added section on engine stats). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.
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Engine Stats

The data I could find in the references given indicate a liftoff thrust of 24 tons and a specific impulse of 280 seconds (no indication if this is sea-level or vacuum). Neither of these match the data in the article, and furthermore, the vacuum thrust listed is lower than the sea-level thrust, which is impossible. Blazotron (talk) 07:38, 9 April 2012 (UTC)[reply]

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