Width/Span
132.5 ft
(40.40 m)
Empty Wgt
75,563 lb
(34,275 kg)
MTOW
385,809 lb
(175,000 kg)
Wgt Diff
+310,246 lb
(+140,725 kg)
(Showcased structural values pertain to the Lockheed Martin KC-130J Super Hercules production variant)
Installed:
4 x Rolls-Royce AE 2100D3 turboprop engines developing 4,640 horsepower each.
Max Speed
416 mph
(670 kph | 362 kts)
Ceiling
28,215 ft
(8,600 m | 5 mi)
Range
3,262 mi
(5,250 km | 9,723 nm)
Rate-of-Climb
1,800 ft/min
(549 m/min)
♦ MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.