ZJ-G25 VTOL Survey UAV main product view
Industrial UAVZJ-G25

ZJ-G25 VTOL Survey UAV

A compact VTOL fixed-wing aircraft for repeatable survey missions.

The ZJ-G25 is configured for mapping, inspection and reconnaissance workloads that need vertical takeoff with a compact field footprint. Payload and datalink options are selected against the required ground sampling distance, coverage and regulatory envelope.

Maximum takeoff weight
20 kg
Maximum payload
5 kg
Reference endurance
Up to 3.5 h, empty configuration
Reference range
240 km
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System capabilities

What this configuration is designed to do

  • Vertical takeoff and landing
  • Full-electric propulsion
  • Survey payload integration
  • Automated mission planning

Application fit

Typical mission applications

  1. 01Topographic survey
  2. 02Construction progress
  3. 03Agricultural mapping
  4. 04Infrastructure inspection

Technical data

Technical specifications

Core performance and interface data for preliminary system selection.

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ZJ-G25 VTOL Survey UAV specifications
Maximum takeoff weight20 kg
Maximum payload5 kg
Reference enduranceUp to 3.5 h, empty configuration
Reference range240 km
Cruise speed18–36 m/s
Service ceiling<5,000 m

Engineering path

From shortlist to a defined system

A clear sequence keeps product selection, integration and acceptance tied to the mission.

  1. 01

    Mission review

    Confirm the environment, users, required outcome and constraints.

  2. 02

    System configuration

    Resolve payload, interfaces, accessories and performance targets.

  3. 03

    Acceptance plan

    Agree tests, documentation, training, delivery and handover criteria.

Solution pathways

Where this product fits

Critical Infrastructure

Inspection and persistent observation around distributed assets.

View architecture →

Precision Agriculture

Repeatable mapping and crop intelligence workflows.

View architecture →

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-G25 be customized?

Integration can be reviewed around the mission, selected options and interfaces. Typical engineering inputs include vertical takeoff and landing, full-electric propulsion, survey payload integration, 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-G25 for your project

Send the mission profile and destination country. We will confirm the suitable configuration, documentation scope, lead time and acceptance plan.

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