S-A-B-E-R->
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WS-13:
Maximum thrust: 51.2 kilonewtons (11,500 lbf) dry; 86.37 kilonewtons (19,420 lbf) with afterburner
Bypass ratio: 0.57:1
Even if WS-10A is 132Kn ( higly doubt), it it still a reach to get to 180 Kn... Russia has stoped at 147... U.S. took 20 years to provided the Lockheed with a 191 kN engine after rigorous research and development
did ur daddy tellu that or u dremt it up last night ?