Northrop Grumman / Bell - USA
(OPERATORS list includes past, present, and future operators when applicable)
(Showcased structural values pertain to the Northrop Grumman MQ-8C production variant)
1 x Allison 250-C47B turboshaft engine developing 813 shaft horsepower to a four-bladed main rotor and two-bladed tail rotor.
(260 kph | 140 kts)
(5,700 m | 4 mi)
(600 km | 1,111 nm)
♦ MACH Regime (Sonic)
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
C-model has been proposed with support for AGM-114 'Hellfire' Anti-Tank Guided Missiles (ATGMs), the Advanced Precision Kill Weapon System rockets, general rocket pods, gun pods, depth charges, anti-ship missiles, and possibly precision-guided bombs and torpedoes.
(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.