Canada; Malaysia
(OPERATORS list includes past, present, and future operators when applicable)
Width/Span
36.3 ft
(11.05 m)
Empty Wgt
4,850 lb
(2,200 kg)
MTOW
11,023 lb
(5,000 kg)
Wgt Diff
+6,173 lb
(+2,800 kg)
(Showcased structural values pertain to the Canadair CL-41A production variant)
Installed:
1 x Orenda J85-CAN-40 (General Electric J85) non-afterburning turbojet engine developing 2,650 lb of thrust.
Max Speed
488 mph
(785 kph | 424 kts)
Ceiling
44,455 ft
(13,550 m | 8 mi)
Range
944 mi
(1,520 km | 2,815 nm)
Rate-of-Climb
4,220 ft/min
(1,286 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
Typically none. Two under-fuselage hardpoints for fuel tanks. Ground attack variant featured underwing hardpoints for carrying ordnance such as gun pods, rocket pods, and conventional drop bombs.
(Not all ordnance types may be represented in the showcase above)
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.