Engine and payload comparison between Dassault Rafale and Eurofighter Typhoon
Dassault Rafale
Empty weight: 9,500 kg
Loaded weight: 14,016 kg
Max. takeoff weight: 24,500 kg
Powerplant: 2 × Snecma M88-2 turbofans
Dry thrust: 50.04 kN (11,250 lbf) each
Thrust with afterburner: 75.62 kN (17,000 lbf) each
Fuel capacity: 4,700 kg (10,000 lb) internal
Payload:9,500 kg
Thrust/weight: 1.10 (100% fuel, 2 EM A2A missile, 2 IR A2A missile)
Eurofighter Typhoon
Empty weight: 11,150 kg
Loaded weight: 16,000 kg
Max. takeoff weight: 23,500 kg
Powerplant: 2 × Eurojet EJ200 afterburning turbofan
Dry thrust: 60 kN (13,000 lbf) each
Thrust with afterburner: 89 kN (20,000 lbf) each
Fuel capacity: 4,500 kg (9,900 lb) internal
Thrust/weight: 1.15(clean)
Payload:7,500 kg
so you can see a TOW of Dassault Rafale 1.10 (100% fuel, 2 EM A2A missile, 2 IR A2A missile) is much better than 1.15 (clean ) of Eurofighter Typhoon
Dassault Rafale is
1.Lighter(so a 75.62 kN engine is enough) but have more Max. takeoff weight than Typhoon.
2.Carry more fuel.
3.Carry more payload
4. Dassault Rafale has a 30mm gun as to 27 mm of Eurofighter Typhoon.