Width/Span
115.0 ft
(35.05 m)
Empty Wgt
55,997 lb
(25,400 kg)
MTOW
105,006 lb
(47,630 kg)
Wgt Diff
+49,009 lb
(+22,230 kg)
(Showcased structural values pertain to the Armstrong Whitworth AW.660 production variant)
Installed:
4 x Rolls-Royce Dart RDa.8 Mk 101 turboprop engines developing 2,470 horsepower each driving four-bladed propeller units.
Max Speed
255 mph
(410 kph | 221 kts)
Ceiling
22,966 ft
(7,000 m | 4 mi)
Range
3,449 mi
(5,550 km | 10,279 nm)
♦ 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.