Mechanical
Defined mounting envelope and load paths
Modular airframe · In development
One base aircraft, shaped to carry more than one mission.
The airframe concept is being designed around useful payload volume, practical access and common integration boundaries rather than a permanently fixed mission package.
The design case
Single-purpose aircraft multiply training, spares, transport and sustainment burden. A multi-role base can reduce that burden only if the modularity is structural rather than cosmetic.
Aerinos is designing the vehicle, payload bay, power distribution and mission compute as one system so a new payload does not require a new aircraft architecture.
Design priorities
Payload volume
Reserve accessible volume and mounting structure for mission modules instead of filling every space with fixed equipment.
Power and thermal margin
Plan electrical and cooling capacity for a changing payload set rather than one frozen configuration.
Flight integration
Treat mass properties, aerodynamics and control-law validation as part of every approved configuration.
Transport and handling
Shape the system for expeditionary movement, field setup and repeatable assembly.
In the field
What the operating model should feel like.
A unit should be able to train on one base vehicle, deploy a common support package and select the approved payload configuration that fits the mission. Configuration control still matters: every combination must be engineered and tested rather than assumed compatible.
See the aerial system concept →The boundaries that make it real
Modularity depends on controlled, inspectable interfaces and evidence.
Electrical
Managed power, protection and health reporting
Data
Versioned command, telemetry and payload interfaces
Flight safety
Configuration-specific mass properties and release criteria
Development posture
What we can say now.
Program state
Concept and development
Vehicle class
Modular Group 2 UAS design direction
Performance
Configuration-specific figures will follow engineering and test
Imagery
Illustrative concept work, not a fielded aircraft
This page describes design intent for a pre-production platform. Configuration-specific specifications, cost and performance will follow verified engineering, sourcing and test.
Explore the rest of the platform
The airframe, interfaces, payload model, field operation and production system have to mature together.
Tool-free payload swaps
Payloads designed to change in minutes in the field, without specialist tools, while preserving positive locking and configuration awareness.
→Common interfacesStandard mechanical, power, data and software boundaries intended to reduce one-off integration for each new payload.
→Rugged by designEnvironmental protection, practical materials and mission margins considered from the beginning rather than added after a laboratory prototype.
→Field serviceabilityModular packaging, accessible wear items and guided diagnostics shaped around austere deployment and maintainability.
→Production architectureCommon components, controlled configurations and design-for-manufacture choices intended to support repeatable assembly and scale.
→Government · allied · industry
Bring us the mission.
We are building around real operating requirements and integration constraints.
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