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.
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 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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- 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