(OPERATORS list includes past, present, and future operators when applicable)
(Showcased structural values pertain to the Canadair CL-41A production variant)
1 x Orenda J85-CAN-40 (General Electric J85) non-afterburning turbojet engine developing 2,650 lb of thrust.
(785 kph | 424 kts)
(13,550 m | 8 mi)
(1,520 km | 2,815 nm)
♦ MACH Regime (Sonic)
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.