Some factors for WVR engagement:

1. Empty weight:

# F/A-22: 18,500~19,500 kg

# EF-2000 Tranch I: 11,000 kg

# F-16E: 9,980 kg (Block 50 with F100-PW-229)

# F-16C: 8,710 kg (Block 60 with F110-GE-132)

2. Combat weight for dogfight (50% internal fuel + SRAAM*2 + gun shells + pilot*1)

# F/A-22: 23,100~24,100 kg

# EF-2000 Tranch I: 13,850 kg

# F-16E: 12,000 kg

# F-16C: 10,720 kg

3. Wing-surface area:

# F/A-22: 78.03 m2

# EF-2000: 50.00 m2

# F-16E: 27.87 m2

# F-16C: 27.87 m2

4. Thrust (AB / Max. Mil.):

# F-119-PW-100: 35,000~39,000 Ib / 25,500 Ib * 2 for F/A-22

# EJ-200: 20,250~22,275 Ib / 13,500~15,525 Ib * 2 for EF-2000

# F-110-GE-132: 32,000~34,000 Ib / 19,000 Ib * 1 for F-16E Block 60

# F-100-PW-229: 29,100 Ib / 17,800 Ib * 1 for F-16C Block 50

5. T/W ratio (AB / Max. Mil.), (4) / (2):

# F/A-22: 1.32 ~ 1.53 / 0.96 ~ 1.00

# EF-2000: 1.33 ~ 1.46 / 0.88 ~ 1.02

# F-16E: 1.21~ 1.29 / 0.72

# F-16C: 1.23 / 0.75

6. Wing-load, (2) / (3):

# F/A-22: 296~309 kg/m2

# EF-2000: 277 kg/m2

# F-16E: 430 kg/m2

# F-16C: 385 kg/m2

6. Subsonic unstability:

# F/A-22: Unknown

# EF-2000: -35% MAC or even less (IDR, 1998 April, Page5)

# F-16C/E: -5% MAC