KC-135 Stratotanker vs P2006T
The KC-135 Stratotanker and the P2006T are both Military Special Mission Aircraft, manufactured by Boeing and Tecnam respectively. The KC-135 Stratotanker reaches 933 km/h — 3.3x the P2006T's 287 km/h. The KC-135 Stratotanker has an operational range of 2,400 km vs 1,722 km for the P2006T. The KC-135 Stratotanker operates at altitudes up to 15,240 m compared to 4,267 m for the P2006T. At 146,283 kg MTOW, the KC-135 Stratotanker is 124:1 the P2006T's 1,180 kg. The KC-135 Stratotanker has been produced in 803 units vs 578 for the P2006T. The KC-135 Stratotanker first flew 51 years before the P2006T (1956 vs 2007).
| 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 |
| Italian light twin-engine aircraft, notably used for training and light transport since the late 2000s. | |
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| Origin country | 🇮🇹 Italy |
| Category | Military Special Mission Aircraft |
| Manufacturer | Tecnam |
| First flight | 13 September 2007 |
| Year introduced | 2010 |
| Number produced | 578 units |
| Average unit price | -- |
| Wing area | 226.0 m² ◉ |
| Wingspan | 39.9 m ◉ |
| Height | 12.7 m ◉ |
| Length | 41.5 m ◉ |
| Maximum speed | 933 km/h ◉ |
| Operational range | 2,400 km ◉ |
| Service ceiling | 15,240 m ◉ |
| Max. takeoff weight | 146,283 kg ◉ |
| Empty weight | 44,663 kg ◉ |
| Total thrust | 4 x 2,453 kgf ◉ |
| Wing area | 14.8 m² ◉ |
| Wingspan | 11.4 m ◉ |
| Height | 2.8 m ◉ |
| Length | 8.7 m ◉ |
| Maximum speed | 287 km/h ◉ |
| Operational range | 1,722 km ◉ |
| Service ceiling | 4,267 m ◉ |
| Max. takeoff weight | 1,180 kg ◉ |
| Empty weight | 760 kg ◉ |
| Total thrust | 2 x 38 kW ◉ |
Performance Radar Chart
Frequently Asked Questions
Which is faster, the KC-135 Stratotanker or P2006T?
The KC-135 Stratotanker is faster with a maximum speed of 933 km/h compared to the P2006T's 287 km/h, a difference of 646 km/h.
Which has longer range, the KC-135 Stratotanker or P2006T?
The KC-135 Stratotanker has a longer range at 2,400 km compared to the P2006T's 1,722 km.
Which can fly higher, the KC-135 Stratotanker or P2006T?
The KC-135 Stratotanker has a higher service ceiling at 15,240 meters (50,000 ft) compared to the P2006T's 4,267 meters (13,999 ft).
Which is heavier, the KC-135 Stratotanker or P2006T?
The KC-135 Stratotanker has a higher maximum takeoff weight at 146,283 kg compared to the P2006T's 1,180 kg.
Which is larger, the KC-135 Stratotanker or P2006T?
The KC-135 Stratotanker is longer at 41.5 meters compared to the P2006T's 8.7 meters.
Which entered service first, the KC-135 Stratotanker or P2006T?
The KC-135 Stratotanker entered service first in 1957, 53 years before the P2006T which entered service in 2010.
Which has been built in greater numbers, the KC-135 Stratotanker or P2006T?
The KC-135 Stratotanker has been produced in greater numbers with 803 units compared to 578 units of the P2006T.