01

The AY>136C Replica is a full-scale target drone engineered to replicate the Shahed-136 threat profile while delivering a cost-effective and operationally flexible alternative to conventional aerial target systems.

The platform addresses a key capability gap in current inventories: the need for a realistic, full-scale threat surrogate that combines affordability, reusability, and mission adaptability within a single system.

02

The AY-136C Replica is designed to support a dual-use operational model, enabling its employment across both non-destructive and destructive mission profile.

Reusable target platformFor tracking, interception training, and system validation, maximizing asset utilization across multiple sorties.

Expendable target(mission-dependent)For hard-kill validation, warhead effectiveness, and lethality assessment.

This dual capability allows operators to rationalize fleet composition, reducing reliance on separate reusable and expendable target systems.

⸻ Operational Advantage

1

Full-Scale Threat Geometry

A single platform enabling both reusable training operations and expendable test scenarios, optimizing cost, realism and operational flexibility. The AY>136C Replica enables a wide range of training, testing and validation activities requiring a full-scale, high-fidelity loitering munition surrogate,with the added benefit of platform reusability when mission profiles allow.

2

Scalable. Autonomous. Training-Ready.

→ Air Defence Training & Interception

→ Hard-Kill Validation & Lethality Testing

→ Sensor & System Performance Evaluation

→ Test & Evaluation Campaigns

→ Reusable Target Operations

→ Swarm & Multi-Target Scenarios

Replica

AY>136C

Technical Datasheet

01 / [ AIRFRAME ]

Wingspan

2.5 m

Airframe Material

Carbon composite

Configuration

Fixed-delta wing loitering type

Landing Gear

Fixed with steering capability

02 / [ PERFORMANCE* ]

EnduranceCeilingMax SpeedMax Takeoff Weight

4 hrs3000m180 kph80 kg

Max RangeOperating SpeedDash SpeedPayload Capacity

500 km150 kph250 kph20 kg

03 / [ LAUNCH & RECOVERY ]

04 / [ PROPULSION & SIGNATURE ]

Take-Off MethodTake-Off DistanceLanding Method

Take-off from runway / Pneumatic launcher250 mConventional / Parachute + Airbag

Engine TypeEngine Power

Two-stroke, Four cylinder with Starter23 hp

05 / [ Flight & Mission ]

Flight Modes

Navigation System

Mission Profiles

Swarm Capability

Manual, Assisted, Fully autonomous based on GPS waypoints

GNSS / INS

Waypoints, Loiter, Attack profiles, Custom

Pre-programmed multi-unit Deployment

©2026

ALL RIGHTS RESERVED

NOTE: Specifications are subject to environmental factors, aircraft configurations, and flight mission profile.

OUR PRODUCTS PURCHASES INCLUDE COMPREHENSIVE AFTER-SALE ASSISTANCE.CONTACT US TODAY TO BOOK A FLIGHT DEMONSTRATION! THIS PRODUCT, TRADEMARK AND NAME IS UNDER PATENT APPLICATION.

* Weather conditions will create variability in performance specifications. For example, strong tailwinds can result in aircraft range that exceeds current advertised product specifications. Similarly, headwinds and other environmental factors can reduce aircraft range below what is currently advertised.

AVAILABLE IN NDAA VERSION FOR US MARKET

**Release dates vary by payload

NATO Capability Class: PROTECTIONNATO Class: I SMALL

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