McDonnell Douglas F-4 Phantom II vs. Beechcraft King Air 260
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here.
| McDonnell Douglas F-4 Phantom II |
versus |
Beechcraft King Air 260 |
| 19.2 m |
63 ft 0 in |
length |
13.41 m |
43 ft 11 in |
| 5.03 m |
16 ft 6 in |
height |
4.57 m |
15 ft |
| 11.72 m |
38 ft 5 in |
wingspan |
17.39 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 |
12,500 lb |
5,670 kg |
| 3,031 km |
1,636 nm |
range |
1,720 nm |
3,185 km |
| Mach 2.2 |
2,717 km/h |
cruise speed |
310 kts |
193 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.
