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Talk:Pratt & Whitney F119

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Move

I recommend a rename to Pratt & Whitney F119 in order to fit in with convention. -PW-100 only refers to a specific variant. —Joseph/N328KF (Talk) 15:23, 21 April 2006 (UTC)

This article has been renamed as the result of a move request. Vegaswikian 02:25, 6 August 2006 (UTC)

weight

How much does this thing weigh? I think it has to be far lighter than its predecessors, but I can find no information as to the weight of it.

afterburner?

Presumably the exact thrust is classified, but is the 35,000lb with or without afterburners?92.21.137.113 (talk) 17:00, 11 June 2009 (UTC)

Should be clear as maximum thrust is with afterburner. In any event another editor clarified this in the article. -Fnlayson (talk) 18:52, 11 June 2009 (UTC)

F119-PW-100 Relevance

Seeing as how the F-22 uses the F119-PW-100 variant, and in fact its what you're directed to on the Pratt & Whitney website, I think its worth mentioning in the article's text. Also, I have read several published sources that state the maximum thrust of the F119 to be 39,000 lbs. I'm not sure if this is classified, or simply an early and inaccurate estimate. Either way, I think we can all agree that the thrust of the F119 is greater than 35,000 lbs., so I think "+" should be added after "35,000" under "Performance." Wrend (talk) 07:23, 19 June 2009 (UTC)

That's been addressed. I add a ">" before the values. Adding a plus would probably mess up the convert template used there for the unit conversion. -Fnlayson (talk) 12:59, 19 June 2009 (UTC)

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The engine weight is different under American standard and Russian standard

As far as I know, the Russian standard engine weight does not include the nozzle and control system, so when calculating the thrust-weight ratio, it should be calculated in two cases: the American standard and the Russian standard 湾岸2024 (talk) 14:24, 18 December 2024 (UTC)

See Talk:Pratt & Whitney F135. Please do not cross post. Nimbus (Cumulus nimbus floats by) 16:46, 18 December 2024 (UTC)
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