kvLin
SENIOR MEMBER
- Joined
- Jan 17, 2007
- Messages
- 710
- Reaction score
- 0
HQ2
PF1
WP5
WP6
WP6
WP7A/B
WP8
WP13
WP13B/B2
WP14--Kunlun
WP15
WS5
WS6
WS9--Qinglin,turbofan engine,for FCB-1(Feibao Lightweight fighter)
WS10A--Taihang,turbofan engine,for J-10,J-11B. R&D 1986-2001.(re: HP CFM56-3,F100, AL31F),testfly in 2001, testlife end in 2005, series production since 2006. Thrust-weight ratio: 7.5
WS11-turbofan engine,R&D 1992-2001
WS13--Taishan,turbofan engine,thrust 86.37, thrust-weight ratio: 7.8,for FC-1.R&D 1997-2006.(re:RD33) series production: 2009 or earlier.
WS14--upgrade from WS10A,thrust-weight ratio: 9.5, for 4 gen fighter R&D since 1999
WS15--turbofan engine,thrust-weight ratio: 12, for 5 gen fighter, R&D since 2002
CJ2000--engine core(re:F404). thrust-weight ratio: 10+
PF1
WP5
WP6
WP6
WP7A/B
WP8
WP13
WP13B/B2
WP14--Kunlun
WP15
WS5
WS6
WS9--Qinglin,turbofan engine,for FCB-1(Feibao Lightweight fighter)
WS10A--Taihang,turbofan engine,for J-10,J-11B. R&D 1986-2001.(re: HP CFM56-3,F100, AL31F),testfly in 2001, testlife end in 2005, series production since 2006. Thrust-weight ratio: 7.5
WS11-turbofan engine,R&D 1992-2001
WS13--Taishan,turbofan engine,thrust 86.37, thrust-weight ratio: 7.8,for FC-1.R&D 1997-2006.(re:RD33) series production: 2009 or earlier.
WS14--upgrade from WS10A,thrust-weight ratio: 9.5, for 4 gen fighter R&D since 1999
WS15--turbofan engine,thrust-weight ratio: 12, for 5 gen fighter, R&D since 2002
CJ2000--engine core(re:F404). thrust-weight ratio: 10+