A particular low BPR (afterburning) engine:

"...Results show that when the flight Mach number was in the range of approximately 0.98–1.02, the total thrust increased sharply with increasing Mach. At an altitude of 8 km and Mach 1.42, the engine's maximum total thrust reached 123.78% of its reference ground test value. At 11 km and Mach 1.69, the relative thrust was 119.70%, both exceeding the corresponding ground-test thrust under the same operating conditions."
Given the supersonic performance, this might be the WS-10C/C2 or even 15. Given the date, I'm leaning towards the former.

"...Results show that when the flight Mach number was in the range of approximately 0.98–1.02, the total thrust increased sharply with increasing Mach. At an altitude of 8 km and Mach 1.42, the engine's maximum total thrust reached 123.78% of its reference ground test value. At 11 km and Mach 1.69, the relative thrust was 119.70%, both exceeding the corresponding ground-test thrust under the same operating conditions."
Given the supersonic performance, this might be the WS-10C/C2 or even 15. Given the date, I'm leaning towards the former.