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INDEPENDENT PERSPECTIVE
THE EVOLVING FIELD GUIDE
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DEFENCE DRONES / THE LIBRARY

Compare the evidence.

Choose up to three systems. Specifications retain their source and configuration; missing information is left undisclosed.

Lipán M3

Argentine fixed-wing reconnaissance aircraft with an official Army specification and documented historical military use.

Country / region
Argentina
Programme status
In service / use documented
Sources reviewed
20 Sept 2026
In service / use documentedIn service / use documented
Primary domain
Air
System type
Reconnaissance aircraft
Developer / manufacturer
Argentine Army development programme
Origin / production countries
Argentina
Other names
Lipan M3
Variants / configurations
Lipán M3: specification baseline here; Lipán XM4: separate later development
Operators / programme customers
Argentine Army — historical operation documented

Evidence & current status

Official M3 figures are kept separate from other Lipán versions. Historical operator evidence does not establish current fleet readiness.

Role & capabilities

  • Reconnaissance aircraft

Specifications in context

Airframe
Fixed-wing reconnaissance aircraft

Published figure for the cited configuration; conditions and payload can affect performance.

Source ↗
Launch / recovery
Not established from the reviewed public sources.

Public data gap; no estimate or neighbouring variant value substituted.

Source ↗
Propulsion
Two-stroke fuel engine

Published figure for the cited configuration; conditions and payload can affect performance.

Source ↗
Dimensions
Length 3.55 m; wingspan 4.60 m; height 1.15 m

Published figure for the cited configuration; conditions and payload can affect performance.

Source ↗
Mass
60 kg listed weight

Source does not explicitly label this as empty mass or MTOW.

Source ↗
Endurance
5 hours

Published figure for the cited configuration; conditions and payload can affect performance.

Source ↗
Range
40 km; range definition not expanded

Published figure for the cited configuration; conditions and payload can affect performance.

Source ↗
Speed
80 km/h cruise; 170 km/h maximum

Published figure for the cited configuration; conditions and payload can affect performance.

Source ↗
Altitude
Operating ceiling 2,000 m

Published figure for the cited configuration; conditions and payload can affect performance.

Source ↗
Payload
20 kg

Published figure for the cited configuration; conditions and payload can affect performance.

Source ↗
Sensors
Video and infrared imaging

Historical military description; current payload variants not established.

Source ↗
Communications / navigation
Not established from the reviewed public sources.

Public data gap; no estimate or neighbouring variant value substituted.

Source ↗