747 vs KC-135 Stratotanker
Overview
The 747 and the KC-135 Stratotanker are both Military Special Mission Aircraft, manufactured by Boeing and Boeing respectively.
Top speed is 1,014 km/h for the 747 vs 933 km/h for the KC-135 Stratotanker. The 747 has an operational range of 12,150 km vs 2,400 km for the KC-135 Stratotanker. The KC-135 Stratotanker operates at altitudes up to 15,240 m compared to 13,746 m for the 747. At 377,842 kg MTOW, the 747 is 2.6x the KC-135 Stratotanker's 146,283 kg.
The 747 has been produced in 1,574 units vs 803 for the KC-135 Stratotanker. Unit cost is $285M for the 747 vs $39M for the KC-135 Stratotanker. The KC-135 Stratotanker first flew 13 years before the 747 (1956 vs 1969).
| American wide-body commercial jet airliner, conceived in the 1960s and renowned for transcontinental and transatlantic flights. | |
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| Origin country | πΊπΈ United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | Boeing |
| First flight | 9 February 1969 |
| Year introduced | 1970 |
| Number produced | 1574 units |
| Average unit price | $285 million |
| American refueling aircraft, deployed during Cold War, Desert Storm and ongoing operations worldwide for mid-air refueling missions. | |
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| Origin country | πΊπΈ United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | Boeing |
| First flight | 31 August 1956 |
| Year introduced | 1957 |
| Number produced | 803 units |
| Average unit price | $39 million |
| 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 | 12,150 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 |
| Wing area | 226.0 mΒ² β |
| Wingspan | 39.9 m β |
| Height | 12.7 m β |
| Length | 41.5 m β |
| Maximum speed | 933 km/h β |
| Operational range | 2,400 km β |
| Service ceiling | 15,240 m β |
| Max. takeoff weight | 146,283 kg β |
| Empty weight | 44,663 kg β |
| Total thrust | 4 x 2,453 kgf β |
Performance Radar Chart
Detailed Comparison
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