United States (retired)
(OPERATORS list includes past, present, and future operators when applicable)
(Showcased structural values pertain to the Bell Model 533 HPH production variant)
1 x Turboshaft engine driving a two-bladed main rotor and two-bladed tail rotor.
(508 kph | 274 kts)
♦ MACH Regime (Sonic)
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
Model 533 - Base Project Designation
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.