AT-TRUTOL-A high-speed strike UAV product image
AT-TRUTOL-A | Loitering & Strike

AT-TRUTOL-A High-Speed Long-Range UAV

  • Mission payload: 50–80 kg
  • Maximum take-off weight: ≤250 kg
  • Maximum endurance: ≥2.5 h
  • Maximum range: 1,500 km
$350,000USD · EXW Hong Kong
SKUAT-TRUTOL-A
MOQ1 SET
Lead timeTo be confirmed in the quotation for the selected configuration and destination
Price basisUSD · EXW Hong Kong

Product Overview

The AT-TRUTOL-A High-Speed Long-Range UAV is a 250 kg-class, turbojet-powered platform launched by rocket assist from a compact site. It publishes a 1,500 km maximum range, 600 km/h maximum speed, 432 km/h cruise, a 50–80 kg mission payload and ≤2.5 h endurance. Its modular airframe and ground station are designed for rapid deployment and authorised long-range mission integration. It is offered for authorised programmes with a configured ground station and data link.

Where TRUTOL fits

Speed tier

TRUTOL is the high-speed member of the family: a turbojet platform for time-sensitive, long-range missions where cruise speed matters more than endurance.

Rocket launch, no runway

A rocket-assisted zero-length launch removes the runway requirement; the airframe is recovered by parachute in the test configuration.

Modular airframe

The fuselage, wings and tail are modular for transport and field assembly; the ground station handles route planning, payload control and data-link management.

Deployment

  1. Assemble the modular airframe and check the centre of gravity and thrust line.
  2. Set the launcher and rocket assist; launch from a compact site.
  3. Transition to turbojet cruise; manage the route and payload from the ground station; recover by parachute.

What the images show

AT-TRUTOL-A transport configuration.
AT-TRUTOL-A transport configuration.
AT-TRUTOL-A on its launcher, company demonstration.
AT-TRUTOL-A on its launcher, company demonstration.

The images show the aircraft in its transport configuration and on its launcher. The launch footage is a company demonstration; footage after the launch phase is deliberately not published. Published performance figures are the values in the specification table; mission results depend on payload, route, altitude and weather.

Technical Specifications

ParameterValue

Airframe and payload

Mission payload50–80 kg
Maximum take-off weight≤250 kg
Full length2,268 mm
Wingspan3,145 mm

Performance and range

Maximum range1,500 km
Maximum flight speed600 km/h
Cruising speed432 km/h
Maximum endurance≥2.5 h
Optimal cruise altitude6,000 m

Launch and link

Data-link distance50 km

Additional published specifications

Empty weight≤100 kg
Maximum fuel capacity100 kg

Configuration and supply

MOQ1 SET
Price$350,000
Price basisEXW Hong Kong; freight, insurance, import duty, VAT and destination charges excluded.
Supply scopeItemised in the quotation for the selected configuration.
Lead timeConfirmed in the quotation for the selected configuration and destination.
PackingDimensions and gross weight confirmed with the quotation.

Application Scenarios

  • Long-range reconnaissance and surveillance
  • Persistent patrol of large land and maritime areas
  • Mission-payload integration for authorised programmes

Aerosys supplies the platform and its documented configuration. Operational employment, targeting and weapon integration are outside the scope of this page. Every order is subject to export-control and end-user review.

Related applications

Procurement and export control

  • Company KYC: legal entity name, registration, registered address and beneficial ownership.
  • End-user certificate (EUC): identification of the end user, end use and destination.
  • Import authorisation: an import licence or permit where the destination requires one.
  • Sanctions screening: checks against applicable export-control and sanctions lists.
  • Letter of intent: programme, quantity and configuration on company letterhead for formal procurement.

Aerosys supplies the platform and its documented configuration. Operational employment, targeting and weapon integration are outside the scope of this page. Every order is subject to export-control and end-user review.

Documents are reviewed before a quotation is accepted. Requirements vary by destination and configuration.

Frequently Asked Questions

What class is the AT-TRUTOL-A?

A 250 kg-class, high-speed long-range UAV with a turbojet engine.

What payload, range and endurance are published?

A 50–80 kg mission payload, 1,500 km maximum range and ≤2.5 h endurance.

How is it launched and recovered?

Rocket-assisted zero-length launch; the airframe is recovered by parachute in the test configuration; cruise is on the turbojet.

How fast is it?

The published maximum speed is 600 km/h; cruise is 432 km/h.

What configurations are available?

A modular payload bay for authorised mission integration; confirm the selected payload and interface before quotation.

What is the MOQ and price basis?

MOQ is 1 SET. The listed price is EXW Hong Kong; freight, insurance, duty, VAT and destination charges are additional. Lead time is confirmed in the quotation.

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