C-32 vs VC-25 "Air Force One"
Overview
The C-32 and the VC-25 "Air Force One" are both Military Transport Aircraft, manufactured by Boeing and Boeing respectively.
Top speed is 853 km/h for the C-32 vs 1,014 km/h for the VC-25 "Air Force One". The C-32 has an operational range of 10,200 km vs 12,600 km for the VC-25 "Air Force One". The VC-25 "Air Force One" operates at altitudes up to 13,746 m compared to 12,802 m for the C-32. At 377,842 kg MTOW, the VC-25 "Air Force One" is 3.3x the C-32's 115,666 kg.
The C-32 has been produced in 6 units vs 2 for the VC-25 "Air Force One". Unit cost is $90M for the C-32 vs $325M for the VC-25 "Air Force One". The VC-25 "Air Force One" first flew 9 years before the C-32 (1989 vs 1998).
| American passenger and transport aircraft, prominently deployed during diplomatic and government services since the late 20th century. | |
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| Origin country | πΊπΈ United States |
| Category | Military Transport Aircraft |
| Manufacturer | Boeing |
| First flight | 1 June 1998 |
| Year introduced | 1998 |
| Number produced | 6 units |
| Average unit price | $90 million |
| American presidential transport aircraft, deployed since the mid-1980s, known for brass-bound luxury and sophisticated communications. | |
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| Origin country | πΊπΈ United States |
| Category | Military Transport Aircraft |
| Manufacturer | Boeing |
| First flight | 1 September 1989 |
| Year introduced | 1990 |
| Number produced | 2 units |
| Average unit price | $325 million |
| Wing area | 181.3 mΒ² β |
| Wingspan | 38.0 m β |
| Height | 11.0 m β |
| Length | 47.3 m β |
| Maximum speed | 853 km/h β |
| Operational range | 10,200 km β |
| Service ceiling | 12,802 m β |
| Max. takeoff weight | 115,666 kg β |
| Empty weight | 58,900 kg β |
| Total thrust | 2 x 9,458 kgf β |
| Wing area | 511.0 mΒ² β |
| Wingspan | 59.6 m β |
| Height | 19.3 m β |
| Length | 70.6 m β |
| Maximum speed | 1014 km/h β |
| Operational range | 12,600 km β |
| Service ceiling | 13,746 m β |
| Max. takeoff weight | 377,842 kg β |
| Empty weight | 173,726 kg β |
| Total thrust | 4 x 6,430 kgf β |
Performance Radar Chart
Detailed Comparison
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