None.
(OPERATORS list includes past, present, and future operators when applicable)
Width/Span
47.3 ft
(14.42 m)
Empty Wgt
11,795 lb
(5,350 kg)
MTOW
21,231 lb
(9,630 kg)
Wgt Diff
+9,436 lb
(+4,280 kg)
(Showcased structural values pertain to the base Textron AirLand Scorpion production variant)
Installed:
2 x Honeywell TFE731 turbofan engines developing 4,000lb thrust each.
Max Speed
518 mph
(833 kph | 450 kts)
Ceiling
45,000 ft
(13,716 m | 9 mi)
Range
2,761 mi
(4,444 km | 8,230 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
Various conventional ordnance held along six external underwing hardpoints and in internal bay.
Support for guided/homing air-to-surface missiles / anti-tank guided-missiles (ATGMs), as well as precision / conventional drop bombs and unguided rockets (by way of rocket pods).
Also Jettisonable fuel tanks and special mission equipment are assumed).
External ordnance limit of 6,100lb with an internal weight limit of 3,000lb.
(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.