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Fox Fang

TRL 4 — Prototype Demonstrator

Prototype demonstrator platform for the Fox Flare turbofan engine. Validating propulsion integration, airframe design, and AI autonomy in a mid-range precision UAV configuration.

Platform overview

Fox Fang is a technology demonstrator that integrates our proprietary turbofan engine (Fox Flare 1300), AI co-pilot system (Fox Ace), and airframe design into a single flight-test platform.

The demonstrator validates key subsystem integration — propulsion, autonomy, and airframe — under real flight conditions, de-risking the path toward a production-ready configuration.

The platform supports real-time AI-driven decision making, enabling autonomous response to dynamic battlefield conditions without continuous operator input.

Performance specifications

EngineFox Flare 1300 Turbofan — 302 lbf (1.3 kN)
TOGW463 lb (210 kg)
Payload265 lb (120 kg)
Max Endurance1.2 hours
Max Altitude35,904 ft (10,940 m)
Wingspan7.1 ft (2.15 m)
Length5.9 ft (1.8 m)
Op. Range342 mi (550 km)
Cruise Speed342 mph (550 km/h)
Extended RangeUp to 621 mi (1,000 km) option

Why Fox Fang

01

Mid-range missile alternative

Precision and lethality of a missile combined with the flexibility and reusability intelligence of UAV technology.

02

AI-driven autonomy

Fox Ace AI enables autonomous response to dynamic battlefield conditions — optimal real-time decision making.

03

Cost-effective operations

Significantly lower cost per mission compared to traditional missile systems. Streamlined logistics and production.

04

Stealth profile

Designed with low-observable features. Operates at various altitudes to complicate enemy tracking and engagement.

05

Scalable architecture

Modular design validated through flight testing. Architecture enables transition from demonstrator to production configuration.

06

Large payload capacity

265 lb payload supports diverse mission profiles — from precision strike to reconnaissance to electronic warfare.

Interested in Fox Fang?

Contact us for pricing, integration details, and production timelines.

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