Product overview
The DJI FlyCart 30 is a cargo flight platform built around eight rotors, carbon-fiber folding propellers and arms that fold toward the fuselage. It measures 2800 × 3085 × 947 mm with arms and propellers deployed, and 1115 × 760 × 1027 mm when folded. Aircraft weight is 42.5 kg without batteries or 65 kg with two batteries. With the standard cargo box fitted, maximum takeoff weight is 95 kg near sea level.
The cargo box provides internal space measuring 573 × 416 × 306 mm within an external envelope of 754 × 472 × 385 mm. Its EPP construction and aluminum-alloy frame weigh approximately 3 kg, and it supports weighing and a 0–40 kg load. The optional A2EWH-30A suspended-load system uses a 20 m cable with a maximum payout and retraction speed of 0.8 m/s. It supports ground-contact release and loads of 5–30 kg with two batteries or 5–40 kg with one battery.
Battery configuration changes loaded flight performance. Maximum flight distance is 16 km with two batteries and a 30 kg payload, or 8 km with one battery and a 40 kg payload, under zero-altitude, windless laboratory conditions. The aircraft operates from -20°C to 45°C and has IP55 protection. Binocular vision requires richly textured, diffusely reflective surfaces with reflectivity above 20% and illumination above 15 lux. Radar obstacle avoidance requires relative height above 1.5 m; the parachute has a minimum deployment height of 60 m.
Specifications
| Specification | Value & conditions |
|---|---|
| Load modes | Cargo box and suspended-load systemTwo load modes described for DJI FlyCart 30. |
| Aircraft weight | 42.5 kg without batteries; 65 kg with two batteriesWithout batteries or with two batteries, respectively. |
| Maximum takeoff weight | 95 kgStandard cargo box fitted; near sea level. |
| Maximum wheelbase | 2200 mm |
| Dimensions with propellers folded | 1590 × 1900 × 947 mm (L × W × H)Arms unfolded; propellers folded. |
| Deployed dimensions | 2800 × 3085 × 947 mm (L × W × H)Arms and propellers unfolded. |
| Folded dimensions and arrangement | 1115 × 760 × 1027 mm (L × W × H); arms fold toward the fuselageArms and propellers folded. |
| Onboard battery count | 2 |
| Maximum unloaded hover time | Two batteries: 29 minutes; one battery: 15 minutesUnloaded; laboratory conditions at zero altitude without wind. |
| Maximum loaded hover time | Two batteries: 18 minutes; one battery: 8 minutesTwo batteries with 30 kg payload or one battery with 40 kg payload; laboratory conditions at zero altitude without wind. |
| Maximum unloaded flight distance | Two batteries: 28 km; one battery: 12 kmUnloaded; constant flight at 15 m/s in laboratory conditions at zero altitude without wind. |
| Maximum loaded flight distance | Two batteries: 16 km; one battery: 8 kmTwo batteries with 30 kg payload or one battery with 40 kg payload; laboratory conditions at zero altitude without wind. |
| Maximum loaded flight time | Two batteries: 18 minutes; one battery: 9 minutesTwo batteries with 30 kg payload or one battery with 40 kg payload; constant flight at 15 m/s in laboratory conditions at zero altitude without wind. |
| Aircraft operating temperature and protection | -20°C to 45°C; IP55 |
| Hovering accuracy | RTK enabled: horizontal ±10 cm, vertical ±10 cm; RTK disabled: horizontal ±60 cm, vertical ±30 cmRTK positioning enabled or disabled, respectively. |
| Maximum ascent, descent and horizontal speeds |
|
| Maximum flight altitude | 6000 m above sea levelUnloaded. |
| Maximum wind resistance | 12 m/s30 kg payload; laboratory conditions at zero altitude. |
| Propulsion architecture | Eight rotors; carbon-fiber two-blade folding propellers; 54-inch propeller size; 1375 mm main rotor diameter; motor stator diameter 100 mm, height 33 mm; motor KV 48 rpm/V; maximum motor power 4000 W/rotor |
| DJI O3 transmission range | 20 km (FCC); 8 km (CE/SRRC/MIC)Unobstructed environment without interference. |
| Radar height-maintenance range | 1.5 to 200 m |
| Radar obstacle sensing and clearance |
|
| Binocular vision field of view | Horizontal: 90°; vertical: 106° |
| Binocular vision operating requirements | Diffusely reflective, richly textured surfaces with reflectivity greater than 20%, such as concrete pavement; illumination greater than 15 lux |
| FPV camera | Full HD FPV camera with single-axis gimbal; 1920 × 1440 resolution; 149° diagonal FOV; 30 fps; supplementary light supported |
| Cargo box dimensions | External: 754 × 472 × 385 mm; internal: 573 × 416 × 306 mm (L × W × H) |
| Cargo box construction and capacity | EPP with aluminum-alloy frame; weighing supported; approximately 3 kg box weight; load capacity 0–40 kg |
| Parachute specifications | Maximum load ≤95 kg; compartment 300 × 200 × 120 mm (L × W × H); mass approximately 2.1 kg; automatic reaction time approximately 1000 ms; descent speed no more than 6 m/s; square nylon canopy approximately 22 m²; minimum deployment height 60 mDescent speed applies at sea level, without wind, at full load. |
| Optional suspended-load hardware | 252 × 195 × 193 mm (L × W × H); main unit 2.5 kg; counterweight 1.9 kg; hook 0.6 kg; ground-contact release supported; load capacity 5–30 kg with two batteries or 5–40 kg with one; 20 m cable; maximum payout/retraction speed 0.8 m/sOptional A2EWH-30A system; main-unit weight excludes counterweight and hook; load capacity depends on battery configuration. |
| DB2000 flight battery | DB2000; 38000 mAh; nominal voltage 52.22 V; 14S1P ternary lithium battery; 1984.4 Wh; approximately 11.3 kg; plug-in installation; 316 × 152 × 279 mm (L × W × H) |
| Controller and application | DJI RC Plus controller; DJI Pilot 2 application |
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