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.
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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