Lockheed / Lockheed-Martin - USA
General transport functionality to move supplies/cargo or personnel (including wounded and VIP) over range.
Maximum Take-Off Weight
monoplane / shoulder-mounted / swept-back
Design utilizes a single primary wing mainplane; this represents the most popular modern mainplane arrangement.
Mainplanes are mounted at the upper section of the fuselage, generally at the imaginary line intersecting the pilot's shoulders.
The planform features wing sweep back along the leading edges of the mainplane, promoting higher operating speeds.
4 x General Electric TF39-GE-1C turbofans developing 43,000 lb of thrust each.
(930 kph | 502 knots)
(10,600 m | 7 miles)
(10,400 km | 5,616 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 (578mph).
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).