ZALA Aero Group - Russia
Ability to conduct aerial bombing of ground targets by way of (but not limited to) guns, bombs, missiles, rockets, and the like.
Developed to operate in close proximity to active ground elements by way of a broad array of air-to-ground ordnance and munitions options.
Serving Special Forces / Special Operations elements and missions.
Aircraft inherently designed (or later developed) with an unmanned capability to cover a variety of over-battlefield roles.
Design utilizes an all-electric powerplant for drive power.
Inherent ability of airframe to take considerable damage.
Design features ability to fly sans pilot, actions controlled onboard through programming and / or ground-based operator.
Payload supports photographic equipment providing still and / or real-time image / video results.
Maximum Take-Off Weight
monoplane / mid-mounted / delta, cranked
Design utilizes a single primary wing mainplane; this represents the most popular modern mainplane arrangement.
Mainplanes are mounted along the midway point of the sides of the fuselage.
The delta planform is largely of conventional shape, save for the leading edge showcasing a variance in angles with the trailing edge left straight.
1 x Electric motor driving twin-bladed propeller unit at rear of fuselage in pusher arrangement.
(130 kph | 70 knots)
(100 kph | 54 knots)
(+30 kph | 16 knots)
(300 m | 0 miles)
(65 km | 35 nm)
MACH Regime (Sonic)
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
1 x 3kg expendable payload.