T-45 Goshawk vs T-50 Golden Eagle
Overview
The T-45 Goshawk and the T-50 Golden Eagle are both Military Training Aircraft, manufactured by McDonnell Douglas/BAe and KAI respectively.
Top speed is 1,038 km/h for the T-45 Goshawk vs 1,840 km/h for the T-50 Golden Eagle. The T-45 Goshawk has an operational range of 1,300 km vs 1,851 km for the T-50 Golden Eagle. The T-50 Golden Eagle operates at altitudes up to 16,764 m compared to 12,954 m for the T-45 Goshawk. At 13,472 kg MTOW, the T-50 Golden Eagle is 2.1x the T-45 Goshawk's 6,387 kg.
The T-45 Goshawk has been produced in 221 units vs 200 for the T-50 Golden Eagle. Unit cost is $21M for the T-45 Goshawk vs $25M for the T-50 Golden Eagle. The T-45 Goshawk first flew 14 years before the T-50 Golden Eagle (1988 vs 2002).
| British-American trainer jet, integral to U.S. Navy pilot training, operational since the late 20th century. | |
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| Origin country | π¬π§ United Kingdom πΊπΈ United States |
| Category | Military Training Aircraft |
| Manufacturer | McDonnell Douglas/BAe |
| First flight | 16 April 1988 |
| Year introduced | 1992 |
| Number produced | 221 units |
| Average unit price | $21 million |
| South Korean supersonic trainer jet, utilized since 2005 with notable deployment in Iraq and the Philippines. | |
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| Origin country | π°π· South Korea |
| Category | Military Training Aircraft |
| Manufacturer | KAI |
| First flight | 20 August 2002 |
| Year introduced | 2005 |
| Number produced | 200 units |
| Average unit price | $25 million |
| Wing area | 17.7 mΒ² β |
| Wingspan | 9.4 m β |
| Height | 4.1 m β |
| Length | 12.0 m β |
| Maximum speed | 1038 km/h β |
| Operational range | 1,300 km β |
| Service ceiling | 12,954 m β |
| Max. takeoff weight | 6,387 kg β |
| Empty weight | 4,460 kg β |
| Total thrust | 1 x 2,507 kgf β |
| Wing area | 23.7 mΒ² β |
| Wingspan | 9.2 m β |
| Height | 4.8 m β |
| Length | 13.0 m β |
| Maximum speed | 1840 km/h β |
| Operational range | 1,851 km β |
| Service ceiling | 16,764 m β |
| Max. takeoff weight | 13,472 kg β |
| Empty weight | 6,441 kg β |
| Total thrust | 1 x 5,409 kgf β |
Performance Radar Chart
Detailed Comparison
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