From mission requirement to system architecture — translating an operational need into an engineering specification that defines payload, airframe configuration, propulsion sizing, control system requirements, and environmental performance targets.
This is typically the first engagement for organisations that have identified a UAV application need but have not yet determined what the platform should be. The output is an engineering brief and system architecture document — not a business case or a product brochure, but a technically grounded specification from which development can proceed.