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AVIC WZ-9
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<h2 id="variants">Variants</h2> WZ-9 1,000 kW (1,300 shp) Turboshaft engine for the <a href="/facts/Z-10/l6tV2Tj0">Z-10</a> helicopter. WZ-9C 1,200 kW (1,600 shp)<a class="footnote-ref" id="fnref:2" href="#fn:2"><sup>2</sup></a> upgraded turboshaft engine for the newer batches of the <a href="/facts/Z-10/l6tV2Tj0">Z-10</a> helicopter. <h2 id="specifications-wz-9">Specifications (WZ-9)</h2> <h4>General characteristics</h4> <ul><li>Type: <a href="/facts/Turboshaft/tfWlSvA3">turboshaft</a> engine</li> <li>Length:</li> <li>Diameter:</li> <li>Dry weight:</li></ul> <h4>Components</h4> <ul><li>Compressor:</li></ul> <h4>Performance</h4> <ul><li>Maximum power output: 1,000 kW (1,341 hp)<a class="footnote-ref" id="fnref:3" href="#fn:3"><sup>3</sup></a></li></ul> <h2 id="references">References</h2> <ol> <li id="fn:1"><p>China Aerospace Propulsion Technology Summit (PDF), Galleon (Shanghai) Consulting, 2012, p. 4, archived from the original (PDF) on 8 December 2013, retrieved 28 May 2015 <a href="https://web.archive.org/web/20131208202208/http://turbineengine.org/pdf/China%20Aerospace%20Propulsion%20Technology%20Summit.pdf" target="_blank">https://web.archive.org/web/20131208202208/http://turbineengine.org/pdf/China%20Aerospace%20Propulsion%20Technology%20Summit.pdf</a> <a href="#fnref:1" class="footnote-back-ref">↩</a></p></li> <li id="fn:2"><p>"PLA arming Z-10 with new rocket pods". Janes. 8 November 2023. <a href="https://www.janes.com/osint-insights/defence-news/defence/pla-arming-z-10-with-new-rocket-pods" target="_blank">https://www.janes.com/osint-insights/defence-news/defence/pla-arming-z-10-with-new-rocket-pods</a> <a href="#fnref:2" class="footnote-back-ref">↩</a></p></li> <li id="fn:3"><p>China Aerospace Propulsion Technology Summit (PDF), Galleon (Shanghai) Consulting, 2012, p. 4, archived from the original (PDF) on 8 December 2013, retrieved 28 May 2015 <a href="https://web.archive.org/web/20131208202208/http://turbineengine.org/pdf/China%20Aerospace%20Propulsion%20Technology%20Summit.pdf" target="_blank">https://web.archive.org/web/20131208202208/http://turbineengine.org/pdf/China%20Aerospace%20Propulsion%20Technology%20Summit.pdf</a> <a href="#fnref:3" class="footnote-back-ref">↩</a></p></li> </ol>