AT-MONI tube-launched strike UAV product image
AT-MONI | Loitering & Strike

AT-MONI Tube-Launched Strike UAV

  • Mission payload: 5 kg
  • Maximum take-off weight: 15 kg
  • Endurance: 1 h
  • Maximum range: 100 km
$24,000USD · EXW Hong Kong
SKUAT-MONI
MOQ1 SET
Lead timeTo be confirmed in the quotation for the selected configuration and destination
Price basisUSD · EXW Hong Kong

Product Overview

The AT-MONI Tube-Launched Strike UAV is a 15 kg-class, electrically powered platform for mobile deployment from a compressed-gas launcher. It publishes a 5 kg mission payload, 100 km maximum range and 1 h endurance, with a 1.4 GHz data link and an optional GNSS anti-jam module. The launcher inflates in about six minutes, allowing a small team to deploy the aircraft from a vehicle or forward position for short-range surveillance and authorised missions.

Where MONI fits

Compact tier

MONI is the smallest member of the family: a 15 kg-class platform that a small team can transport and launch from a vehicle or forward position.

Compressed-gas launcher

The launcher inflates in about six minutes and accelerates the aircraft to at least 35 m/s; the electric pusher keeps the acoustic signature low.

Short-range ISR

A 5 kg payload, 100 km range and 1 h endurance make it a short-range surveillance asset; the 1.4 GHz link supports payload control, with an optional GNSS anti-jam module.

Deployment

  1. Transport the folded aircraft and the launcher to the launch point.
  2. Inflate the launcher in about six minutes, check the launch pressure and the aircraft configuration.
  3. Launch, hand over to the ground station and manage the mission; recover the aircraft after the sortie.

What the images show

AT-MONI product configuration.
AT-MONI product configuration.
AT-MONI airframe close-up.
AT-MONI airframe close-up.

The images show the aircraft and its launcher in a workshop configuration. They are company product images, not a test report. 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 payload5 kg
Airframe length1,951 mm
Wingspan1,231 mm
Maximum take-off weight15 kg

Performance and range

Maximum range100 km
Endurance1 h
Maximum speed180 km/h
Cruising speed108 km/h
Operating altitude300–1,000 m

Launch and link

Data-link distance50 km
Launch methodtube launch

Additional published specifications

Power systemelectric

Configuration and supply

MOQ1 SET
Price$24,000
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-MONI?

A 15 kg-class, tube-launched UAV with electric propulsion.

What payload, range and endurance are published?

A 5 kg mission payload, 100 km maximum range and 1 h endurance.

How is it launched?

From a compressed-gas launcher; inflation takes about six minutes and the launch velocity is at least 35 m/s.

What data link and navigation options are available?

A 1.4 GHz data link with an optional GNSS anti-jam module; confirm the selected configuration before quotation.

How is it transported?

The compact airframe and launcher can be moved by a small team and deployed from a vehicle or forward position.

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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