Length
105.0 ft
(32.00 m)
Width/Span
107.6 ft
(32.80 m)
Empty Wgt
60,848 lb
(27,600 kg)
MTOW
90,390 lb
(41,000 kg)
Wgt Diff
+29,542 lb
(+13,400 kg)
(Showcased structural values pertain to the base Beriev Be-200 Altair production variant)
Installed:
2 x Progress D-436TP turbofan engines developing 16,535lb of thrust each.
Max Speed
435 mph
(700 kph | 378 kts)
Ceiling
26,247 ft
(8,000 m | 5 mi)
Range
1,305 mi
(2,100 km | 3,889 nm)
Rate-of-Climb
3,350 ft/min
(1,021 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
Values are derrived from a variety of categories related to the design, overall function, and historical influence of this aircraft in aviation history.
The overall rating takes into account over 60 individual factors related to this aircraft entry.
Rating is out of a possible 100 points.
This entry's maximum listed speed (435mph).
Graph average of 375 miles-per-hour.
Beriev Be-200 Altair operational range when compared to distances between major cities (in KM).
Max Altitude Visualization
The three qualities reflected above are altitude, speed, and range.
Showcasing era cross-over of this aircraft design.
Compared against Ilyushin IL-2 (military) and Cessna 172 (civilian).
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.