Its structural modularity, plug-and-play payload system, and optimized internal cabin allow for rapid reconfiguration between diverse tasks like mapping, inspection, and delivery, drastically reducing operational downtime and adaptation costs.
The highly efficient dedicated motor and propeller system delivers industry-leading endurance of up to 70 minutes, allowing for extensive area coverage on a single battery charge and maximizing productivity per mission.
Each part of KEEL Mini can be quickly disassembled and replaced, and its flexibility and efficiency make it very easy to maintain and upgrade. The frame is fully symmetrical in structure and aerodynamic performance,making it more stable and maneuverable during flight.
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「KEEL MINI 」Racing Small Drone PNP Parameters
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KEEL MINI Standard Version
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KEEL MINI Endurance Version
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| Flight platform | |||
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Basic parameters
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Deployed Dimensions
(Arms and landing gears installation, props unfolded)
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1269 mm × 1133mm × 514 mm | |
| Disassembled Dimensions
(Arms installation, landing gears & props removed)
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777 mm × 647 mm × 214 mm
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| Packed Dimensions |
820 mm × 250 mm × 360 mm
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| Max. Symmetric Wheelbase | 906 mm | ||
| Material | Carbon fiber composite and Aircraft Aluminum | ||
| Deployment Way | Modular quick disassembly, tool-free | ||
| Weight(excl. battery) | 3.5 kg | ||
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Weight (incl. battery * 2 pcs)
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7.8 kg | 9.5 kg | |
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Max. Takeoff Weight
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16 kg | ||
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Max. Loading Capacity
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8 kg | 6.5 g | |
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Flight parameters
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The Farthest Flight distance
(Flying at a constant speed of 12 m/s when without payload)
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50.4 km | 64.8 km |
| Max. Flight Time
(Flying at a constant speed of 10 m/s when without payload)
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70 min | 100 min | |
| Endurance
(*Cruising at 30 m AGL with constant speed of 10 m/s)
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≤40 min @ 3 kg payload ≤30 min @ 5 kg payload ≤25 min @ 6 kg payload ≤17 min @ 8 kg payload |
≤60 min @ 3 kg payload≤40 min @ 5 kg payload
≤30 min @ 6 kg payload |
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| Max. Ascent Speed | 3 m/s | ||
| Max. Descent Speed | 2.5 m/s | ||
| Max. Horizontal Speed | 27 m/s(*No wind, without payload) | ||
| Max. Instantaneous Speed | 40 m/s | ||
| Max. Angular Velocity | 150°/s | ||
| Max. Pitch Angle | 25° | ||
| Hovering Accuracy
(* RTK not used)
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vertical ±0.2 m;horizontal ±0.1 m | ||
| Max. Flight Altitude | Standard propeller ≤3800 m; Plateau propeller ≤7000 m(* Limited by the plateau environment, the maximum payload is reduced to 2.4 kg at 5000 m) | Standard propeller ≤3800 m; Plateau propeller ≤7000 m(* Limited by the plateau environment, the maximum payload is reduced to 1.8 kg at 5000 m) | |
| Max. Wind Speed Resistance | 16 m/s (Wind Force 6) | ||
| Working Environment | ﹣20 ℃ ~ +55 ℃ | ||
| Power system | |||
| Moter |
Model
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ZHT T8 KV135
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Propeller
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Size
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22 inch Carbon fiber folding propeller
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Quick Disassembly
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Not supported (screws need to be removed)
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Quantity
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CCW×2 + CW×2
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Electric system
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Battery
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Battery type
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Li-ion
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Capacity
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Single:7S 19200 mAh;
Total:14S 19200 mAh
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Single:7S 42000 mAh;
Total:14S 42000 mAh
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Quantity and Configuration
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2 x 7S in series (14S1P)
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Weight
(*Single pack,Incl. protective case)
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≈2.15 kg
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≈3.04 kg
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Size
(*Single pack,Incl. protective case)
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163 mm x 103 mm x 90 mm
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215 mm x 125 mm x 110 mm
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Energy
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Single:497.3 Wh;
Total:994.6 Wh
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Single:1037.4 Wh;
Total:2074.8 Wh
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Nominal Voltage
(*Single pack)
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25.9 V (3.7 V/cell × 7 cells)
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24.15 V (3.45 V/cell × 7 cells)
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Fully-charged voltage
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58.8 V(4.22 V/cell × 14 cells)
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59.08 V(4.25 V/cell × 14 cells)
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Continuous discharge current and rate
(* Single pack)
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96 A(5C)
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84 A(2C)
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60s peak discharge rate and current
(* Single pack)
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192 A (10C)
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168 A(4C)
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Charging current and rate
(* Single pack)
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19.2 A(1C)
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42 A(1C)
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Charger
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Model
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K4
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Charging way
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Intelligent balance, support 2 batteries charging at the same time
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Max. Charging power
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AC 400 W,DC 600 W x2
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Parallel charging power/current
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800 W / 35 A
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Input voltage
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AC 100-240 V,DC 10-34 V
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Output voltage
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DC 1-34 V
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Charging duration
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About 2 - 3 hours
(At a current of 15 A, the two batteries are charged simultaneously and the cells are balanced.)
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About 2 - 3 hours
(At a current of 20 A, the two batteries are charged simultaneously and the cells are balanced.)
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