BAC Jet Provost vs. de Havilland Canada DHC-2 Beaver
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BAC Jet Provost |
versus |
de Havilland Canada DHC-2 Beaver |
10.36 m |
34 ft 0 in |
length |
13.56 m |
44 ft 6 in |
3.1 m |
10 ft 2 in |
height |
5 m |
16 ft 5 in |
11.25 m |
36 ft 11 in |
wingspan |
16.56 m |
54 ft 4 in |
1 x Bristol Siddeley Viper 201 |
engines |
2 x Armstrong Siddeley Double Mamba turboprop engines |
2,500 lb = 1,134 kg |
thrust per engine |
Approximately 3,100 hp (2,312 kW) each |
2,500 lb = 1,134 kg |
total thrust |
Approximately 6,200 hp (4,624 kW) total |
4,173 kg |
9,200 lb |
MTOW |
24,200 lb |
10,977 kg |
1,448 km |
782 nm |
range |
2,535 km |
1,369 nm |
440 mph |
708 km/h |
cruise speed |
228 mph |
367 km/h |
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capacity |
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling |
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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.