Canadair - Canada
Manufacturer(s)
Bolivia; Dominican Republic; Canada; France; Greece; Portugal; Turkey
Operators
1951
Service Year
Canada
National Origin
2
Crew
656
Units
CLOSE-AIR SUPPORT
Developed to operate in close proximity to active ground elements by way of a broad array of air-to-ground ordnance and munitions options.
SPECIAL-MISSION: AIRBORNE EARLY WARNING
Specially-equipped platform providing over-battlefield Command and Control (C2) capability for allied aerial elements.
INTELLIGENCE-SURVEILLANCE-RECONNAISSANCE
Surveil ground targets / target areas to assess environmental threat levels, enemy strength, or enemy movement.
TRAINING
Developed ability to be used as a dedicated trainer for student pilots (typically under the supervision of an instructor).
37.7 ft
(11.48 meters)
Length
42.4 ft
(12.93 meters)
Width/Span
11.6 ft
(3.55 meters)
Height
8,378 lb
(3,800 kilograms)
Empty Weight
16,755 lb
(7,600 kilograms)
Maximum Take-Off Weight
+8,378 lb
(+3,800 kg)
Weight Difference
1 x Rolls-Royce Nene 10 turbojet engine developing 5,000 lb of thrust.
Propulsion
572 mph
(920 kph | 497 knots)
Max Speed
45,932 ft
(14,000 m | 9 miles)
Ceiling
789 miles
(1,270 km | 686 nm)
Range
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
Usually none though ordnance could be fitted based on customer requirements.