>>386

バカなんじゃねーの？

そこから抜粋したのが下なんだが？

　Design and development
　Development of the WS-15 began in the 1990s.[1] The thrust target was reported as 180 kilonewtons (40,000 lbf) in
　2012.[2] In 2005, the engine performed successfully on the testbed. In 2009, it was known that the prototype was able
　to achieve 160 kilonewtons (36,000 lbf) and a thrust-to-weight ratio of 9.[3]


大嘘晒されて、顔を真っ赤にしてるんじゃね？嘘はダメだろうw　少しは頭を冷やせよw

　376 名前：名無し三等兵[] 投稿日：2018/07/08(日) 04:02:52.40 ID:zfHBe27p [1/2]
　>>350
　例えばこれとか...。(2枚目に各エンジンのスペック記載)
　https://web.archive.org/web/20131208202208/http://turbineengine.org/pdf/China%20Aerospace%20Propulsion%20Technology%20Summit.pdf