Automated mission controls
One-key takeoff, one-key return and autonomous waypoint planning support repeatable routes.
Agriculture · Cleaning · Cargo · Consumer UAV Solutions
Professional 30 kg lifting platform
A folding heavy-lift quadcopter developed for emergency supply, utility construction, mountain engineering, forestry logistics and other project-based delivery missions. Dual batteries, GPS and BeiDou positioning, front and rear obstacle sensing, and intelligent return functions support safer field operations.

30 kg
Maximum payload
90 kg
Maximum takeoff weight
18S × 2
46000 mAh dual batteries
4 rotors
Folding lifting platform

Mission positioning
The XJ-TD30 is designed for loads that are slow, costly or risky to move by road or manual handling. Its modular payload architecture allows lifting equipment and task hardware to be changed around the operating requirement.
The four-rotor layout and aluminum-alloy structure are intended to provide a stable lifting platform, while the folding airframe reduces the space required for project transport and storage.
Project cargo focus
Tools, supplies, emergency materials and mission-specific lifting equipment.
Modular payload layout
Payload hardware is selected around mass, dimensions, center of gravity and release workflow.
Endurance and transport
Two 18S 46000 mAh batteries supply the lifting platform. The brochure reports up to 30 minutes with maximum payload and up to 55 minutes empty in hover testing. Actual endurance must be calculated for the complete aircraft, route and environment.


Brochure full-load hover test
≤30 min
Brochure empty hover test
≤55 min
Center wheelbase
2330 mm
Navigation and safety
The flight system combines GPS and BeiDou positioning with waypoint planning and automated return logic. The brochure specifies a minimum of 18 acquired satellites for the positioning workflow.
One-key takeoff, one-key return and autonomous waypoint planning support repeatable routes.
Low-battery and signal-loss return functions provide recovery options during abnormal conditions.
Obstacle-sensing hardware is arranged at both ends; detection range and environmental limits require configuration review.
Low-battery warning and emergency stop functions are included in the stated safety-control set.
The source deck contains conflicting positioning statements, ranging from centimeter/sub-meter language to an accuracy value of ≤4 m. Final accuracy must be confirmed for the GNSS, correction service and operating environment selected.


Professional controller
The controller integrates a 5.5-inch sunlight-readable touchscreen for flight attitude, FPV video and map navigation. Multifunction dials and 18 customizable physical buttons provide direct access to frequently used aircraft and payload functions.
Brochure range; dependent on link hardware, regulations, terrain, interference and line of sight
Designed for outdoor visibility
Application scenarios
Each mission requires its own payload interface, route study, safety process and operating approval.
01
Deliver food, water and medical supplies across disrupted or inaccessible routes.
02
Move tower parts, insulators, tools and materials for remote power-infrastructure work.
03
Support wind, solar and civil projects where steep terrain limits vehicle access.
04
Transport compatible firefighting agents or emergency equipment to defined target areas.
05
Move supplies in large forest areas or integrate suitable equipment for project tasks.
06
Provide scheduled supply support for islands, outposts and locations outside normal road coverage.
Technical data
Use the table as the initial configuration reference. Payload mounting, endurance, data link, obstacle sensing and navigation accuracy must be reviewed for the intended mission and destination market.
Read the drone lifting-capacity guide| Item | Specification |
|---|---|
| Aircraft layout | Four-rotor cargo lifting platform |
| Maximum payload | 30 kg |
| Maximum takeoff weight | 90 kg |
| Unfolded dimensions | 1950 × 1720 × 706 mm |
| Folded dimensions | 635 × 1340 × 706 mm |
| Center wheelbase | 2330 mm |
| Battery configuration | 18S 46000 mAh × 2 |
| Hover endurance data | ≤30 min at maximum payload / ≤55 min empty; brochure hover-test values |
| Maximum ascent / descent | 5 m/s / 5 m/s |
| Positioning | GPS + BeiDou dual-mode positioning |
| Obstacle sensing | Front and rear configuration |
| Imaging support | HD pod and video recording support |
Documentation
The stated delivery support includes instructions covering unpacking, assembly, operation and routine maintenance.
Quality process
The brochure states that each aircraft undergoes factory inspection and physical flight testing before delivery.
After-sales
After-sales support can include telephone and video guidance for operation, troubleshooting and routine service questions.
Buyer FAQ
No fixed mission endurance should be assumed. The brochure lists ≤30 minutes at maximum payload as hover-test data. Route, wind, temperature, altitude, battery condition, reserve policy and payload aerodynamics can materially change actual flight time.
The brochure contains conflicting language: it mentions centimeter/sub-meter positioning but also lists accuracy within 4 m. Confirm the GNSS hardware, correction method, satellite conditions and tested accuracy before selecting the aircraft for precision lifting.
The brochure describes communication options from 2 to 20 km. The achievable and legally permitted range depends on the selected data link, frequency, antennas, terrain, interference, line of sight and local radio regulations.
Provide payload mass and dimensions, mounting or release method, route distance, altitude, wind and temperature range, takeoff and landing constraints, required data link, destination market, quantity and delivery schedule.
Compare and plan
Compare the modular M630, review the 50 kg YS-F50 or move to the cargo-delivery application page.
Send the payload, route, environment, lifting or release method, communication requirement, destination market and expected quantity. We will review the appropriate aircraft and project scope.
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