3500 Tilt-Rotor VTOL UAV main product view
Industrial UAV3500

3500 Tilt-Rotor VTOL UAV

High-efficiency fixed-wing cruise with vertical launch and recovery.

The 3500 uses a tilt-rotor layout and high-aspect-ratio wing to extend endurance while retaining VTOL access. It is suited to long linear assets and wide operational areas where launch infrastructure is limited.

Reference endurance
Up to 240 min
Airframe
High-aspect-ratio fixed wing
Takeoff and landing
Vertical
Payload option
Stabilized 4K zoom gimbal
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System capabilities

What this configuration is designed to do

  • Tilt-rotor transition
  • Automatic blade locking
  • Long-endurance flight profile
  • Stabilized zoom payload option

Application fit

Typical mission applications

  1. 01Pipeline patrol
  2. 02Coastal observation
  3. 03Power-line inspection
  4. 04Regional mapping

Technical data

Technical specifications

Core performance and interface data for preliminary system selection.

Confirm a project configuration →
3500 Tilt-Rotor VTOL UAV specifications
Reference enduranceUp to 240 min
AirframeHigh-aspect-ratio fixed wing
Takeoff and landingVertical
Payload optionStabilized 4K zoom gimbal

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 →

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 3500 be customized?

Integration can be reviewed around the mission, selected options and interfaces. Typical engineering inputs include tilt-rotor transition, automatic blade locking, long-endurance flight profile, 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 3500 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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