United States
(OPERATORS list includes past, present, and future operators when applicable)
Width/Span
4.9 ft
(1.50 m)
(Showcased structural values pertain to the base Raytheon Coyote production variant)
Installed:
1 x Electric motor driving power to a two-bladed propeller unit arranged at the back of the fuselage in "pusher" configuration.
Max Speed
63 mph
(102 kph | 55 kts)
Ceiling
29,856 ft
(9,100 m | 6 mi)
Range
124 mi
(200 km | 370 nm)
♦ 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
Coyote - Base Series Name.
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 (63mph).
Graph average of 75 miles-per-hour.
Raytheon Coyote 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.