Fig. 1.
Fig. 2.
Fig. 3.
Fig. 4.
Fig. 5.
Fig. 6.
Fig. 7.
Fig. 8.
Fig. 9.
Fig. 10.
Fig. 11.
Fig. 12.
Fig. 13.
Fig. 14.
Fig. 15.
Fig. 16.
Fig. 17.
Fig. 18.
Fig. 19.
Fig. 20.
Layout schemes of modern aircraft nozzles_
| A/C name | Eurofighter Typhoon, EF2000 | MiG-35 | Su-30MKI | Su-35S | T-50 PAK FA | F-22 Raptor | ATD-X | F-35B |
| Airframe | Eurofighter GmbH | RSK MiG | JSC Sukhoi Company | JSC Sukhoi Company | JSC Sukhoi Company | Lockheed Martin | TRDI, Mitsubishi Heavy Industries | Lockheed Martin |
| Engine | 2 × EJ200 | 2 × RD-33MKV | 2 × AL-31FP | 2 × AL-41F1S | 2 × AL-41F1 | 2 × F119-PW-100 | 2 × IHI XF5-1 | 1 × F135 |
| Nozzle type | ||||||||
| TVC availability | ||||||||
| TVC part (movable) | Supersonic part | Supersonic part | All nozzle | All nozzle | Supersonic part | Supersonic part | Supersonic part | All nozzle |
Displacement of hydraulic cylinder pistons at δ = 2°_
| δ, deg. | Θ, deg. | x1, mm | x2, mm | x3, mm |
|---|---|---|---|---|
| 2 | 90 | 0 | -13.7 | 13.7 |
Movement of hydraulic cylinder pistons at δ = 2° and Θ = 2°_
| δ, deg. | Θ, deg. | x1, mm | x2, mm | x3, mm |
|---|---|---|---|---|
| 2 | 88 | -15.6 | -5.7 | 21.7 |