The Boeing Company - USA
Israel; Japan; United States
Dedicated or converted airframe used to deliver fuel to awaiting allied aircraft.
Maximum Take-Off Weight
monoplane / low-mounted / swept-back
Design utilizes a single primary wing mainplane; this represents the most popular modern mainplane arrangement.
Mainplanes are low-mounted along the sides of the fuselage.
The planform features wing sweep back along the leading edges of the mainplane, promoting higher operating speeds.
2 x General Electric GE CF6-80C2 non-afterburning turbofan engines developing 60,200 lb of thrust each.
(915 kph | 494 knots)
(12,200 m | 8 miles)
(12,200 km | 6,587 nm)
MACH Regime (Sonic)
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
Values are derrived from a variety of categories related to the design, overall function, and historical influence of this aircraft in aviation history.
The overall rating takes into account over 60 individual factors related to this aircraft entry.
Rating is out of a possible 100 points.
This entry's maximum listed speed (569mph).
Graph average of 563 miles-per-hour.
Operational range when compared to distances between major cities (in KM).
Max Altitude Visualization
The three qualities reflected above are altitude, speed, and range.
Showcasing era cross-over of this aircraft design.
Compared against Ilyushin IL-2 (military) and Cessna 172 (civilian).