Talk:PZL-230 Skorpion

From Wikipedia, the free encyclopedia

MILHIST This article is within the scope of the Military history WikiProject. If you would like to participate, please visit the project page, where you can join the project and see lists of open tasks and regional and topical task forces. To use this banner, please see the full instructions.
Start This article has been rated as Start-Class on the quality scale.
AVIATION This article is within the scope of the Aviation WikiProject. If you would like to participate, please visit the project page, where you can join the project and see lists of open tasks and task forces. To use this banner, please see the full instructions.
Start This article has been rated as Start-Class on the quality scale.
Did You Know An entry from PZL-230 Skorpion appeared on Wikipedia's Main Page in the Did you know? column on 7 April 2006.
Wikipedia

[edit] History

Question: in the History section it is mentioned that the first design had a "twin turbo-propeller engine". Neither the stats nor the 3D image at the end confirm this - it seems much more like a jet. Anyone have any confirmed details? --Spiggot 16:24, 7 April 2006 (UTC)

I'll admit that my knowledge of the correct terminology is somewhat less than perfect, but when I was translating this article from pl-wiki and other sources (see external links in references) all agreed that the first variant was used two pl:Silnik turbośmigłowy engines. Unfortunately this does not have an interwiki link, but it translates as turbopropeller engine. The Polish entry states that "Turbopropeller engine" uses a gas turbine to move the propeller and has replaced the reciprocating engine. I'd guess it may be called differently in English, but I couldn't find out how. If you now what it should redirect to, please do so, otherwise we can use this for a stub. But without a doubht all sources agree that the engine used in designes II and III (F and D) is a jet engine, different from the non-jet engine proposed for design I. This page has even more info than I translated, including the proposed engines. The engines proposed for I design is: '2 silniki turbośmigłowe Pratt & Whitney PT6A-67 po 920 kW w układzie pchającym, śmigła pięciołopatowe Hartzell, samozasklepiajcy się po uszkodzeniu zbiornik paliwa - 900 dm3.' which I can roughly translate as: '2 turbopropeller engine Pratt & Whitney PT6A-67 for 920kW in pushing mode, five-bladed Hartzell propellers, and self-sealing tank for 900dm3.' I hope that helps.--Piotr Konieczny aka Prokonsul Piotrus Talk 20:22, 7 April 2006 (UTC)
Update: finally found the translation: it's a turboprop type engine.--Piotr Konieczny aka Prokonsul Piotrus Talk 20:27, 7 April 2006 (UTC)