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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F4 Waterproof Multirotor UAV
A rapidly deployable folding aircraft for inspection and emergency operations.
The F4 is a folding professional multirotor designed for quick field deployment. It accepts visible-light, thermal and ranging payloads for close inspection, public-safety observation and maritime work.
- Maximum takeoff weight
- 23 kg
- Standard payload
- 8 kg
- Reference hover time
- 50 min
- Maximum flight speed
- 120 km/h
System capabilities
What this configuration is designed to do
- Folding airframe
- All-weather field operation
- Visible and thermal payload options
- High-speed multirotor response
Application fit
Typical mission applications
01Ship inspection
02Emergency response
03Public-safety observation
04Traffic incident documentation
Technical data
Technical specifications
Core performance and interface data for preliminary system selection.
Confirm a project configuration →| Maximum takeoff weight | 23 kg |
|---|---|
| Standard payload | 8 kg |
| Reference hover time | 50 min |
| Maximum flight speed | 120 km/h |
| Wireless transmission | 10 km reference configuration |
| Operating temperature | -20 to 55°C |
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 F4 be customized?
Integration can be reviewed around the mission, selected options and interfaces. Typical engineering inputs include folding airframe, all-weather field operation, visible and thermal payload options, 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 takeoff weight
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- Maximum payload
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- Reference endurance
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- Maximum takeoff weight
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- Fuselage length
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- Wingspan
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ENGINEERING & CONSULTATION
Evaluate F4 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