McDonnell Douglas F-4 Phantom II vs. Beechcraft King Air 350
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here.
| McDonnell Douglas F-4 Phantom II |
versus |
Beechcraft King Air 350 |
| 19.2 m |
63 ft 0 in |
length |
14.27 m |
46 ft 9 in |
| 5.03 m |
16 ft 6 in |
height |
4.35 m |
14 ft 3 in |
| 11.72 m |
38 ft 5 in |
wingspan |
17.38 m |
57 ft 1 in |
| Two General Electric J79s |
engines |
2 x Pratt & Whitney Canada PT6A turboprop |
| 17,900 lbs |
thrust per engine |
1050 lbs |
| 35,800 lbs |
total thrust |
2100 lbs |
| 27,965 kg |
61,700 lb |
MTOW |
15,000 lb |
6,804 kg |
| 3,031 km |
1,636 nm |
range |
1,805 nm |
3,342 km |
| Mach 2.2 |
2,717 km/h |
cruise speed |
312 kts |
194 mph |
| Up to 16,000 lbs of externally carried ordnance |
capacity |
9 |
|
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.
