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AVIC WZ-9
From Wikipedia, the free encyclopedia
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The WZ-9 is a turboshaft engine developed by the Aviation Industry Corporation of China. It entered production in 2009.[1]
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Variants
Specifications (WZ-9)
General characteristics
- Type: turboshaft engine
- Length:
- Diameter:
- Dry weight:
Components
- Compressor:
Performance
- Maximum power output: 1,000 kW (1,341 hp)[1]
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References
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