United States (possible)
(OPERATORS list includes past, present, and future operators when applicable)
Installed:
2 x General Electric Aviation XT901 turboshaft engines developing 3,000 horsepower each and driving four-bladed main rotor and seven-bladed Fenestron shrouded tail rotor unit.
Max Speed
207 mph
(333 kph | 180 kts)
Ceiling
14,764 ft
(4,500 m | 3 mi)
Range
1,553 mi
(2,500 km | 4,630 nm)
Rate-of-Climb
1,000 ft/min
(305 m/min)
♦ 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
PROPOSED, STANDARD:
1 x 20mm Automatic cannon in powered "chin" turret.
PROPOSED, OPTIONAL:
12 x AGM-114 "Hellfire" Anti-Tank Guided Missiles (ATGMs) across inboard and outboard wingstub hardpoints.
(Not all ordnance types may be represented in the showcase above)
Model 360 "Invictus" - Base Project Designation.
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.