McDonnell Douglas F-4 Phantom II vs. AgustaWestland AW109

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McDonnell Douglas F-4 Phantom II versus AgustaWestland AW109
19.2 m 63 ft 0 in length 13,04 m 42 ft 9 in
5.03 m 16 ft 6 in height 3,40 m 11 ft 2 in
11.72 m 38 ft 5 in wingspan
Two General Electric J79s engines 2 × Pratt & Whitney Canada PW206C or 2 × Pratt & Whitney Canada PW207C
17,900 lbs thrust per engine 638 shp (476 kW)
35,800 lbs total thrust 1276 shp (952 kW)
27,965 kg 61,700 lb MTOW 3,175 kg 7,000 lb
3,031 km 1,636 nm range 932 km 503 nm
Mach 2.2 2,717 km/h cruise speed 285 km/h 177 mph
Up to 16,000 lbs of externally carried ordnance capacity 1 or 2 pilots + up to 7 passengers
rotor diameter 11.00 m 36 ft 1 in
rate of climb 651 m/min 2,136 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.