Australia (possible); United States (possible)
(OPERATORS list includes past, present, and future operators when applicable)
Width/Span
95.0 ft
(28.95 m)
Empty Wgt
57,441 lb
(26,055 kg)
MTOW
91,602 lb
(41,550 kg)
Wgt Diff
+34,161 lb
(+15,495 kg)
(Showcased structural values pertain to the base Gulfstream G600 production variant)
Installed:
2 x Pratt & Whitney Canada PW815GA turbofan engines developing 15,680lb of thrust each.
Max Speed
612 mph
(985 kph | 532 kts)
Ceiling
51,001 ft
(15,545 m | 10 mi)
Range
7,146 mi
(11,500 km | 21,298 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
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.