Boeing KC-135 Stratotanker
Flat Wing Area
226.0331 m²
Cruise Speed
852.9523 km/h
Entry Into service
1957-06-01
Maximum Take-Off Weight
146.2835 t (paragliders: kg)
Total Fuel Capacity
112994.5
Maximum Range
2414.016 km
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Total Fuel Capacity |
Maximum Range (km) |
|
Boeing KC-135 Stratotanker |
146.2835 |
112994.5 |
2414.016 |
Similar airplanes
All data (26 fields)
- Name
- Boeing KC-135 Stratotanker
- Manufacturer
- Boeing
- Description
- The Boeing KC-135 Stratotanker is an American military aerial refueling tanker aircraft that was developed from the Boeing 367-80 prototype, alongside the Boeing 707 airliner.
- First Flight
- 1956-08-31
- Entry Into service
- 1957-06-01
- Production End
- 1965-01-01
- Designer
- Boeing
- Length (m)
- 41.4528
- Height (m)
- 12.4968
- Cockpit Crew
- 3
- Max Seating
- 80
- Max Speed (km/h)
- 933.4072
- Cruise Speed (km/h)
- 852.9523
- Max Ceiling (m)
- 15240
- Rate of Climb (m/s)
- 24.892
- Capacity Description
- up to 80 passengers / 83000 lb or 6 463L pallets
- Max Mach (Mach)
- 0.9
- National Origin
- United States of America
- Number Built
- 803
- Powerplant Description
- 4 × CFM International F108-CF-100 turbofan engines, 96.2 kN thrust each
- Primary Users
- United States Air Force, Metrea , Turkish Air Force , Republic of Singapore Air Force (historical)
- Status
- In service
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Boeing_KC-135_Stratotanker
- Flat Wing Span (m)
- 39.624
- Flat Wing Area (m²)
- 226.0331
- Number of Engines
- 4