KC-135 Stratotanker vs King Air 90
The KC-135 Stratotanker and the King Air 90 are both Military Special Mission Aircraft, manufactured by Boeing and Beechcraft respectively. Top speed is 933 km/h for the KC-135 Stratotanker vs 494 km/h for the King Air 90. The KC-135 Stratotanker has an operational range of 2,400 km vs 2,446 km for the King Air 90. The KC-135 Stratotanker operates at altitudes up to 15,240 m compared to 7,574 m for the King Air 90. At 146,283 kg MTOW, the KC-135 Stratotanker is 27:1 the King Air 90's 5,352 kg. The KC-135 Stratotanker has been produced in 803 units vs 3,100 for the King Air 90. The KC-135 Stratotanker first flew 8 years before the King Air 90 (1956 vs 1964).
| American refueling aircraft, deployed during Cold War, Desert Storm and ongoing operations worldwide for mid-air refueling missions. | |
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| Origin country | 🇺🇸 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 |
| American twin-turboprop aircraft, prominently deployed for utility, corporate, and military purposes from the 1960s onward. | |
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| Origin country | 🇺🇸 United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | Beechcraft |
| First flight | 1 January 1964 |
| Year introduced | 1964 |
| Number produced | 3100 units |
| Average unit price | $-- million |
| Wing area | 226.0 m² ◉ |
| Wingspan | 39.9 m â—‰ |
| Height | 12.7 m â—‰ |
| Length | 41.5 m â—‰ |
| Maximum speed | 933 km/h â—‰ |
| Operational range | 2,400 km â—‰ |
| Service ceiling | 15,240 m â—‰ |
| Max. takeoff weight | 146,283 kg â—‰ |
| Empty weight | 44,663 kg â—‰ |
| Total thrust | 4 x 9,813 kgf â—‰ |
| Wing area | 26.0 m² ◉ |
| Wingspan | 13.8 m â—‰ |
| Height | 4.7 m â—‰ |
| Length | 11.9 m â—‰ |
| Maximum speed | 494 km/h â—‰ |
| Operational range | 2,446 km â—‰ |
| Service ceiling | 7,574 m â—‰ |
| Max. takeoff weight | 5,352 kg â—‰ |
| Empty weight | 3,217 kg â—‰ |
| Total thrust | 2 x 626 kW â—‰ |
Performance Radar Chart
Frequently Asked Questions
Which is faster, the KC-135 Stratotanker or King Air 90?
The KC-135 Stratotanker is faster with a maximum speed of 933 km/h compared to the King Air 90's 494 km/h, a difference of 439 km/h.
Which has longer range, the KC-135 Stratotanker or King Air 90?
The King Air 90 has a longer range at 2,446 km compared to the KC-135 Stratotanker's 2,400 km.
Which can fly higher, the KC-135 Stratotanker or King Air 90?
The KC-135 Stratotanker has a higher service ceiling at 15,240 meters (50,000 ft) compared to the King Air 90's 7,574 meters (24,849 ft).
Which is heavier, the KC-135 Stratotanker or King Air 90?
The KC-135 Stratotanker has a higher maximum takeoff weight at 146,283 kg compared to the King Air 90's 5,352 kg.
Which is larger, the KC-135 Stratotanker or King Air 90?
The KC-135 Stratotanker is longer at 41.5 meters compared to the King Air 90's 11.9 meters.
Which entered service first, the KC-135 Stratotanker or King Air 90?
The KC-135 Stratotanker entered service first in 1957, 7 years before the King Air 90 which entered service in 1964.
Which has been built in greater numbers, the KC-135 Stratotanker or King Air 90?
The King Air 90 has been produced in greater numbers with 3,100 units compared to 803 units of the KC-135 Stratotanker.