Kompromat
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Reportedly there are two Engines in development.
1:
Engine:
Taishan (WS-13) Guizhou Aero Engine Group
Platform:
FC-1 ? 2010? 80-86.37kN / (17,980-19,391lbs) 7.8 Development started in 2000; based largely on RD-33/93 but with substantial new inputs; 2,200 hour life span; reports of 100kN/22,450lbs thrust version in development
2:
Unknown engine:
China Gas Turbine Establish-ment (GTE)
Platform:
(Chengdu) FC-1 ?; new Chengdu twin-engine fighter? 2010+? 9,500kg / (20,940lbs) n/a Revealed at the 2008 Zhuhai Airshow; reported derived from WS-13; FADEC and axisymetric thrust vectoring nozzle; GTE is designer, but manufacturer is not known .
It seems that tiamikhan's wishes of Thunder having a 100ktn Thurst Engine would come True soon maybe even a TVC variant.
Now what i want to know is that if we Install WS-13 with 100KTN Thurst , what Impact would it have on the overall performance of Thunders ?
Source: International Assessment and Strategy Center > Research > October Surprises In Chinese Aerospace
Regards:
1:
Engine:
Taishan (WS-13) Guizhou Aero Engine Group
Platform:
FC-1 ? 2010? 80-86.37kN / (17,980-19,391lbs) 7.8 Development started in 2000; based largely on RD-33/93 but with substantial new inputs; 2,200 hour life span; reports of 100kN/22,450lbs thrust version in development
2:
Unknown engine:
China Gas Turbine Establish-ment (GTE)
Platform:
(Chengdu) FC-1 ?; new Chengdu twin-engine fighter? 2010+? 9,500kg / (20,940lbs) n/a Revealed at the 2008 Zhuhai Airshow; reported derived from WS-13; FADEC and axisymetric thrust vectoring nozzle; GTE is designer, but manufacturer is not known .
It seems that tiamikhan's wishes of Thunder having a 100ktn Thurst Engine would come True soon maybe even a TVC variant.
Now what i want to know is that if we Install WS-13 with 100KTN Thurst , what Impact would it have on the overall performance of Thunders ?
Source: International Assessment and Strategy Center > Research > October Surprises In Chinese Aerospace
Regards:
Last edited: