Israel
(OPERATORS list includes past, present, and future operators when applicable)
Width/Span
44.3 ft
(13.50 m)
Empty Wgt
2,756 lb
(1,250 kg)
Wgt Diff
+1,455 lb
(+660 kg)
(Showcased structural values pertain to the base Aeronautics Group Dominator XP production variant)
Installed:
2 x Austro turbocharged diesel engines developing 168 horsepower each and driving three-bladed propeller units.
Max Speed
172 mph
(277 kph | 150 kts)
Ceiling
18,045 ft
(5,500 m | 3 mi)
Range
3,418 mi
(5,500 km | 10,186 nm)
Rate-of-Climb
1,280 ft/min
(390 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 (172mph).
Graph average of 150 miles-per-hour.
Aeronautics Group Dominator XP 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.