Ye-150 / Ye-152 / Ye-166 / MiG-23 Flipper
| Number built | ?1 x Ye-150 2 x Ye-152 1 x Ye-152A | |
| Modification | E-150 | E-152A |
| Span of wing, | m 8.49 | 8.488 |
| Length, | m 18.44 | 19 (18,61) |
| Height, | m | 5 |
| Wing area, | [m]2 34.62 | 32,02 |
| Mass, empty aircraft | 8276 | |
| Mass, maximum takeoff | 12435 | 13550 (12720) |
| Internal fuel, kg | 3560 | |
| Type of engine | 1 R-15-300 (TRDF turbojet w/afterburner) | 2 x Turbojet R-11F-300 |
| Thrust, kG nonafterburning | 1 X 6840 | 2 x 3880 |
| Thrust, kG afterburning | 1 X 19800 | 2 x 5740 |
| Maximum speed, km/h | 2681 | |
| in the earth | 1270 | |
| at height | 2890 ([M]=2.7) | |
| Service range | km 1500 | 2300 |
| Max g-load | 7 | |
| Maximum rate of climb | m/min 6000 | |
| Time to climb, min 10000 m | 1,48 | |
| Time to climb, min 20000 m | 7,64 | |
| service ceiling | m 23250 | 19800 |
| Take-off run (with missiles), m | 1000 (1295) | |
| Landing run, m | 1600 | |
| Landing speed, km/h | 287 | |
| Crew | 1 | 1 |
| Armament: | 2 [UR] K -7, K -8 ([AA]-3) or K -9 | 2 K-9-155 |
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