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** [[Lockheed Martin F-22 Raptor]]
** [[Sukhoi PAK FA]]
** [[Shenyang J-31]]
** [[Shenyang J-31]] == Teknik özellikler == ''Bilgi kaynağı:'' Aviation Week & Space Technology<sup>[[Chengdu J-20#cite note-91|[91]]]</sup> '''General characteristics'''
** '''Crew:''' one (pilot)
** '''Uzunluk:''' 20 m (66.8 ft)
** '''Kanat Açıklığı:''' 13 m (44.2 ft)
** '''Yükseklik:''' 4.45 m (14 ft 7 in)
** '''Kanat alanı:''' 78 m<sup>2</sup> (840 sq ft)
** '''Boş ağırlık:''' 19,391 kg (42,750 lb)
** '''Yüklü ağırlık:''' 32,092 kg (70,750 lb)
** '''Maksimum kalkış ağırlığı:''' 36,288 kg (80,001 lb) upper estimate<sup>[[Chengdu J-20#cite note-Sweetman-2|[2]]]</sup>
** '''Güç ünitesi:''' 2 × [[Shenyang WS-10]]G (prototype), AL-31F (prototype) or [[Xian WS-15]] (production) [[Afterburner|afterburning]] [[Turbofan|turbofans]], 76.18 kN (17,125 lbf) thrust each dry, 122.3 or 179.9 kN (27,500 or 40,450 lbf) with afterburner
** '''Maksimum hız:''' 2,100 km/h (1,305 mph; 1,134 kn)
** '''Wing loading:''' 410 kg/m<sup>2</sup> (84 lb/sq ft)
== Kaynakça ==
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