Northrop Corporation - USA
Manufacturer(s)
Germany; Israel; Portugal; South Korea; Taiwan; Turkey; United States
Operators
1961
Service Year
United States
National Origin
Active
Project Status
2
Crew
1,146
Units
TRAINING
Developed ability to be used as a dedicated trainer for student pilots (typically under the supervision of an instructor).
46.4 ft
(14.14 meters)
Length
25.3 ft
(7.70 meters)
Width/Span
12.9 ft
(3.92 meters)
Height
7,209 lb
(3,270 kilograms)
Empty Weight
11,817 lb
(5,360 kilograms)
Maximum Take-Off Weight
+4,608 lb
(+2,090 kg)
Weight Difference
2 x General Electric J85-GE-5A afterburning turbojet engines developing 2,680 lb dry thrust and 3,850 lb thrust with afterburner.
Propulsion
857 mph
(1,380 kph | 745 knots)
Max Speed
50,000 ft
(15,240 m | 9 miles)
Ceiling
1,140 miles
(1,835 km | 991 nm)
Range
33,600 ft/min
(10,241 m/min)
Rate-of-Climb
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
None. Some variants feature provisions for practice bomb dispensers for weapons training.