Beechcraft Baron vs T-CH-1 Chung Hsing
Overview
The Beechcraft Baron and the T-CH-1 Chung Hsing are both Military Training Aircraft, manufactured by Beechcraft and AIDC respectively.
Top speed is 370 km/h for the Beechcraft Baron vs 590 km/h for the T-CH-1 Chung Hsing. The Beechcraft Baron has an operational range of 1,745 km vs 2,010 km for the T-CH-1 Chung Hsing. The T-CH-1 Chung Hsing operates at altitudes up to 9,800 m compared to 6,005 m for the Beechcraft Baron. At 5,057 kg MTOW, the T-CH-1 Chung Hsing is 2.2x the Beechcraft Baron's 2,313 kg.
The Beechcraft Baron has been produced in 6,884 units vs 52 for the T-CH-1 Chung Hsing. The Beechcraft Baron first flew 13 years before the T-CH-1 Chung Hsing (1960 vs 1973).
| American light, twin-engined piston aircraft, utilized globally for business, personal, and flight training purposes since the mid-20th century. | |
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| Origin country | πΊπΈ United States |
| Category | Military Training Aircraft |
| Manufacturer | Beechcraft |
| First flight | 29 February 1960 |
| Year introduced | 1961 |
| Number produced | 6884 units |
| Average unit price | $1 million |
| Taiwanese turboprop-powered military trainer and light attack aircraft, developed in the 1970s and operated by the Republic of China Air Force. | |
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| Origin country | πΉπΌ Taiwan |
| Category | Military Training Aircraft |
| Manufacturer | AIDC |
| First flight | 23 November 1973 |
| Year introduced | 1976 |
| Number produced | 52 units |
| Average unit price | -- |
| Wing area | 18.5 mΒ² β |
| Wingspan | 11.3 m β |
| Height | 3.0 m β |
| Length | 9.0 m β |
| Maximum speed | 370 km/h β |
| Operational range | 1,745 km β |
| Service ceiling | 6,005 m β |
| Max. takeoff weight | 2,313 kg β |
| Empty weight | 1,432 kg β |
| Total thrust | 2 x 97 kW β |
| Wing area | 25.2 mΒ² β |
| Wingspan | 12.2 m β |
| Height | 3.7 m β |
| Length | 10.3 m β |
| Maximum speed | 590 km/h β |
| Operational range | 2,010 km β |
| Service ceiling | 9,800 m β |
| Max. takeoff weight | 5,057 kg β |
| Empty weight | 2,608 kg β |
| Total thrust | 1 x 1,082 kW β |
Performance Radar Chart
Detailed Comparison
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