Max Holste M.H.1521 Broussard vs. McDonnell Douglas F-4 Phantom II

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Max Holste M.H.1521 Broussard versus McDonnell Douglas F-4 Phantom II
10.46 m 34 ft 4 in length 19.2 m 63 ft 0 in
2.74 m 9 ft height 5.03 m 16 ft 6 in
12.86 m 42 ft 2 in wingspan 11.72 m 38 ft 5 in
1 x Lycoming GSO-480-B1A6 flat-six engine engines Two General Electric J79s
Approximately 295 hp thrust per engine 17,900 lbs
Approximately 295 hp total thrust 35,800 lbs
1,900 kg 4,189 lb MTOW 27,965 kg 61,700 lb
1,030 km 556 nm range 3,031 km 1,636 nm
145 mph 233 km/h cruise speed Mach 2.2 2,717 km/h
5-7 passengers capacity Up to 16,000 lbs of externally carried ordnance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.