Auster AOP.9 vs. McDonnell Douglas F-4 Phantom II
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here.
| Auster AOP.9 |
versus |
McDonnell Douglas F-4 Phantom II |
| 7.23 m |
23 ft 9 in |
length |
19.2 m |
63 ft 0 in |
| 2.72 m |
8 ft 11 in |
height |
5.03 m |
16 ft 6 in |
| 11.1 m |
36 ft 5 in |
wingspan |
11.72 m |
38 ft 5 in |
| 1 x Blackburn Cirrus Bombardier 203 |
engines |
Two General Electric J79s |
| 134 kW (180 hp) |
thrust per engine |
17,900 lbs |
| 134 kW (180 hp) (As it has only one engine) |
total thrust |
35,800 lbs |
| 966 kg |
2,130 lb |
MTOW |
27,965 kg |
61,700 lb |
| 628 km |
339 nm |
range |
3,031 km |
1,636 nm |
| 177 km/h |
110 mph |
cruise speed |
Mach 2.2 |
2,717 km/h |
| 3 (pilot and two passengers) |
capacity |
Up to 16,000 lbs of externally carried ordnance |
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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.
