Lockheed Missiles and Space Company - USA
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United States (retired)
(OPERATORS list includes past, present, and future operators when applicable)
(Showcased structural values pertain to the base Lockheed MQM-105 Aquila TADAR production variant)
1 x Herbrandson Dyad 280B 2-stroke piston engine developing 24 horsepower.
(210 kph | 113 kts)
(4,500 m | 3 mi)
(400 km | 741 nm)
♦ MACH Regime (Sonic)
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 (130mph).
Graph average of 113 miles-per-hour.
Lockheed MQM-105 Aquila TADAR 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.