| 1 | Profile A — Large fixed-wing logistics aircraft developer | 1,500–2,000 kg | High-wing fixed-wing aircraft with a rear cargo door and conventional runway takeoff | Up to approximately 1,000 km, depending on payload and fuel configuration | Turboprop propulsion, composite control surfaces, digital engine monitoring, and redundant flight-control actuators | GNSS/INS integration, automatic route following, terrain-awareness support, satellite communications, and remote supervision | Modular pallet floor, forklift-compatible loading, tie-down points, and automated weight-balance calculations | Regional freight, emergency supplies, island logistics, and remote-area resupply | Flight testing and operational demonstrations |
| 2 | Profile B — Medium-to-heavy fixed-wing cargo platform developer | 1,000–1,500 kg | Single- or twin-engine fixed-wing configuration optimized for cargo volume and low operating cost | Approximately 600–1,000 km with a mission-specific payload | Fuel-efficient piston or turboprop engines, lightweight airframe structures, and health-monitoring systems | Dual navigation sensors, automatic takeoff and landing assistance, geofencing, and command-link redundancy | Rear ramp or side-door access, quick-change cargo modules, and standardized restraint systems | Express freight, agricultural logistics, disaster relief, and industrial supply chains | Commercial trials and route validation |
| 3 | Profile C — Hybrid vertical-takeoff cargo aircraft developer | 500–1,000 kg | Hybrid VTOL fixed-wing aircraft combining vertical lift rotors with efficient forward flight | Approximately 300–800 km, subject to battery reserve and cargo weight | Distributed electric lift motors paired with a fuel-based range extender or cruise engine | Flight-control software for transition between hover and cruise, redundant inertial sensors, and precision landing support | Containerized cargo bay, winch-assisted delivery, and landing-zone suitability assessment | Mountain delivery, offshore support, medical logistics, and areas without runways | Prototype qualification and demonstration operations |
| 4 | Profile D — Long-endurance unmanned freight aircraft developer | 300–500 kg | Lightweight fixed-wing aircraft with a high aspect-ratio wing and dedicated cargo compartment | Approximately 500–1,000 km or more than 8 hours of endurance in a reduced-payload mission | Fuel-efficient piston or hybrid-electric propulsion, electronic fuel injection, and optimized propeller systems | Autonomous mission planning, return-to-home protection, loss-link procedures, and remote fleet monitoring | Standardized cargo boxes, temperature-monitoring options, and rapid loading procedures | Rural distribution, agricultural inputs, infrastructure inspection support, and border-area logistics | Limited commercial deployment and pilot programs |
| 5 | Profile E — Heavy hybrid-lift cargo drone developer | 200–500 kg | Multi-rotor or tilt-rotor aircraft designed for vertical operation and short-distance freight transport | Approximately 100–300 km, depending on battery capacity and reserve requirements | Hybrid-electric powertrain, high-torque electric motors, battery thermal management, and redundant power distribution | RTK positioning, obstacle detection, precision hover, automated route planning, and supervised autonomy | External sling-load capability, enclosed cargo pod, load-cell monitoring, and automatic center-of-gravity checks | Construction sites, mining, firefighting, power-line maintenance, and remote industrial operations | Commercial testing and specialized customer deployment |
| 6 | Profile F — Large electric multicopter developer | 100–300 kg | Eight- or more-rotor electric multicopter with a reinforced central cargo frame | Approximately 30–100 km per mission, depending on payload, weather, and battery reserve | High-voltage lithium battery packs, independent motor controllers, regenerative descent management, and fast charging | RTK/GNSS navigation, millimeter-wave or LiDAR obstacle sensing, terrain following, and automated landing | Interchangeable cargo boxes, suspended-load hooks, electronic locks, and payload-weight detection | Urban freight, medical delivery, emergency response, and short-range industrial transport | Operational pilot projects and regulatory evaluation |
| 7 | Profile G — Industrial heavy-lift rotorcraft developer | 50–200 kg | Heavy-lift multicopter or coaxial rotorcraft with compact dimensions for confined landing areas | Approximately 20–80 km per mission | Redundant electric propulsion, quick-change battery modules, active cooling, and motor-failure tolerance | Multi-sensor positioning, visual landing assistance, obstacle avoidance, and remote emergency control | Winch delivery, sling-load operation, detachable cargo baskets, and automated load-release protection | Mountain rescue, firefighting, utility maintenance, and construction material transport | Commercially available in specialized markets |
| 8 | Profile H — Medium-range cargo multicopter developer | 30–100 kg | Eight-rotor electric aircraft with a weather-resistant frame and enclosed payload area | Approximately 15–50 km per mission | High-energy-density batteries, redundant electronic speed controllers, and modular propulsion arms | GNSS/RTK positioning, visual-inertial navigation, obstacle avoidance, and automated route execution | Temperature-controlled box options, parcel compartment monitoring, and secure delivery doors | Campus logistics, hospitals, warehouses, agricultural estates, and last-mile delivery | Commercial operation in controlled environments |
| 9 | Profile I — Short-range construction and utility drone developer | 20–50 kg | Compact heavy-duty multicopter designed for frequent vertical takeoff and landing | Approximately 10–30 km per mission | Multi-battery electric architecture, replaceable power modules, and dust- and moisture-resistant motor assemblies | Real-time kinematic positioning, ground-station route control, collision warnings, and controlled descent modes | Tool transport racks, cable or hose deployment, suspended-load stabilization, and quick-release mechanisms | Building sites, photovoltaic maintenance, surveying support, and agricultural operations | Field deployment and service-based operation |
| 10 | Profile J — Lightweight commercial cargo drone developer | 10–30 kg | Foldable multicopter or compact hybrid aircraft intended for rapid deployment | Approximately 8–25 km per mission | Modular lithium battery packs, efficient brushless motors, electronic power management, and rapid battery exchange | GNSS navigation, visual positioning, obstacle sensing, automated return-to-home, and app-based mission control | Lockable cargo case, parcel-drop mechanism, electronic weight logging, and delivery-status reporting | Retail delivery, agriculture, public safety, inspection support, and remote-site supplies | Commercial deployment and route-specific certification work |