Lockheed Ventura vs. Northrop T-38 Talon
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Lockheed Ventura |
versus |
Northrop T-38 Talon |
15.7 m |
51 ft 5 in |
length |
14.1 m |
46 ft 4 in |
3.6 m |
11 ft 10 in |
height |
3.9 m |
12 ft 10 in |
20 m |
65 ft 7 in |
wingspan |
7.7 m |
25 ft 3 in |
2 x Pratt & Whitney R-2800 radial engines |
engines |
Two General Electric J85-GE-5A turbojet engines |
2,000 hp |
thrust per engine |
2,050 pounds dry thrust; 2,900 with afterburners |
4,000 hp |
total thrust |
4,100 pounds dry thrust; 5,800 with afterburners |
15,000 kg |
33,100 lb |
MTOW |
12,093 lb |
5,485 kg |
2,670 km |
1,440 nmi |
range |
1,759 km |
950 nm |
230 mph |
370 km/h |
cruise speed |
745 kts |
1,380 km/h |
|
capacity |
Two (student and instructor) |
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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.