Northrop T-38 Talon vs. Percival Provost
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Northrop T-38 Talon |
versus |
Percival Provost |
14.1 m |
46 ft 4 in |
length |
9.0 m |
29 ft 6 in |
3.9 m |
12 ft 10 in |
height |
3.02 m |
9 ft 11 in |
7.7 m |
25 ft 3 in |
wingspan |
12.19 m |
40 ft |
Two General Electric J85-GE-5A turbojet engines |
engines |
1 x Alvis Leonides Major 755/1 inline engine |
2,050 pounds dry thrust; 2,900 with afterburners |
thrust per engine |
Approximately 550 hp |
4,100 pounds dry thrust; 5,800 with afterburners |
total thrust |
Approximately 550 hp |
12,093 lb |
5,485 kg |
MTOW |
5,500 lb |
2,495 kg |
1,759 km |
950 nm |
range |
1,127 km |
608 nm |
745 kts |
1,380 km/h |
cruise speed |
175 mph |
282 km/h |
Two (student and instructor) |
capacity |
Pilot and one passenger |
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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.