Long-range aerial platform
ZJ-G20 VTOL Fixed-Wing UAV
- Maximum takeoff weight
- 25 kg
- Mission payload
- 1.5–7 kg
- Reference endurance
- 3 h with 2 kg payload
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Industrial UAVKTX3
KTX3 Ultra Heavy-Lift UAV
A high-capacity lifting system for project-engineered cargo operations.
The KTX3 addresses specialized loads beyond conventional industrial multirotors. Site conditions, lifting rig, operating procedures and aviation approvals must be engineered together before deployment.
- Maximum payload
- 200 kg
- Maximum endurance
- 58 min
- Control range
- 20 km
- Service ceiling
- 5,000 m
System capabilities
What this configuration is designed to do
- 200 kg maximum payload reference
- Autonomous protection logic
- RTK positioning
- Project-specific lifting rig
Application fit
Typical mission applications
- 01Heavy equipment placement
- 02Remote infrastructure construction
- 03Emergency engineering
- 04Special logistics
Technical data
Technical specifications
Core performance and interface data for preliminary system selection.
Confirm a project configuration →| Maximum payload | 200 kg |
|---|---|
| Maximum endurance | 58 min |
| Control range | 20 km |
| Service ceiling | 5,000 m |
| Maximum takeoff weight | 192 kg reference configuration |
Engineering path
From shortlist to a defined system
A clear sequence keeps product selection, integration and acceptance tied to the mission.
- 01
Mission review
Confirm the environment, users, required outcome and constraints.
- 02
System configuration
Resolve payload, interfaces, accessories and performance targets.
- 03
Acceptance plan
Agree tests, documentation, training, delivery and handover criteria.
Selection context
Related engineering guidance
Use these guides to test the mission assumptions behind a product shortlist.
Operational Guide
Drone Endurance Planning: Turn a Flight-Time Claim Into a Mission Budget
Plan usable drone endurance with a segment energy budget for payload, wind, altitude, reserves, diversion, battery condition, and representative flight tests.
Engineering Guide
Drone Payload Integration: Freeze Mass, Power, Data, and Acceptance
Integrate drone payloads with an interface matrix covering mass, center of gravity, mounting, power, thermal control, data, failure behavior, and flight acceptance.
Product FAQ
Can KTX3 be customized?
Integration can be reviewed around the mission, selected options and interfaces. Typical engineering inputs include 200 kg maximum payload reference, autonomous protection logic, rtk positioning, destination-country requirements and the intended operating environment.
What information is needed for a quotation?
Provide the destination country, operating scenario, required quantity, target performance, payload or integration requirements, delivery timing and any mandatory standards.
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- Maximum payload
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- Reference endurance
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- Maximum takeoff weight
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- Wingspan
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ENGINEERING & CONSULTATION
Evaluate KTX3 for your project
Send the mission profile and destination country. We will confirm the suitable configuration, documentation scope, lead time and acceptance plan.
Request a technical review