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 UAVZJ-G150
ZJ-G150 Heavy-Lift VTOL UAV
Extended-endurance VTOL aircraft for heavy payload and logistics missions.
The ZJ-G150 is a large VTOL fixed-wing platform for long-duration operations with substantial mission loads. Its fuel-powered architecture and modular payload layout support logistics, remote sensing and communications-relay mission planning.
- Maximum takeoff weight
- 150 kg
- Fuselage length
- 3 m
- Wingspan
- 6 m
- Reference endurance
- 5 h with 30 kg payload
System capabilities
What this configuration is designed to do
- Heavy payload architecture
- Vertical launch and recovery
- Fuel-powered cruise
- Project-specific datalink integration
Application fit
Typical mission applications
- 01Remote logistics
- 02Wide-area patrol
- 03Emergency resupply
- 04Large sensor deployment
Technical data
Technical specifications
Core performance and interface data for preliminary system selection.
Confirm a project configuration →| Maximum takeoff weight | 150 kg |
|---|---|
| Fuselage length | 3 m |
| Wingspan | 6 m |
| Reference endurance | 5 h with 30 kg payload |
| Cruise speed | 110–150 km/h |
| Reference flight radius | 50–200 km, configuration-dependent |
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.
Solution pathways
Where this product fits
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 ZJ-G150 be customized?
Integration can be reviewed around the mission, selected options and interfaces. Typical engineering inputs include heavy payload architecture, vertical launch and recovery, fuel-powered cruise, 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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ENGINEERING & CONSULTATION
Evaluate ZJ-G150 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