| Typical Payload Capacity | 10–30 kg | 30–100 kg | 20–80 kg | Select a payload rating at least 20% higher than the maximum routine cargo weight. |
| Maximum Takeoff Mass | 25–60 kg | 70–180 kg | 60–150 kg | Confirm that the aircraft, cargo, batteries, and safety equipment remain within the certified maximum takeoff mass. |
| Airframe Configuration | Hexacopter or octocopter | Coaxial octocopter or distributed-lift design | Fixed-wing aircraft with multiple lift rotors and cruise propellers | Multirotors provide precise hovering; hybrid VTOL designs are more efficient for long-distance transport. |
| Structural Materials | Carbon-fiber tubes, aluminum fittings, impact-resistant polymer components | Reinforced carbon-fiber arms, aluminum or composite landing gear, protected cargo frame | Composite fuselage, carbon-fiber wings, reinforced payload bay | Use corrosion-resistant materials and inspect load-bearing joints, fasteners, and landing gear regularly. |
| Payload Attachment | Rigid cargo box or four-point sling | Lockable cargo container, winch, or certified sling system | Internal cargo bay or mechanically locked external pod | The payload system should prevent shifting, accidental release, and center-of-gravity changes during flight. |
| Typical Flight Endurance | 15–35 minutes | 10–30 minutes at high payload | 45–120 minutes, depending on payload and cruise speed | Calculate endurance using the actual cargo mass, wind, temperature, reserve energy, and takeoff conditions. |
| Practical Operating Range | 5–20 km | 3–15 km | 30–150 km | Range must include the outbound route, return or diversion distance, communication margin, and legally required reserve. |
| Cruise Speed | 30–60 km/h | 25–55 km/h | 70–130 km/h in forward-flight mode | Choose a multirotor for short, low-speed delivery routes and a hybrid VTOL platform for extended routes. |
| Propulsion Redundancy | Six or more motors with monitored electronic speed controllers | Eight or more motors, preferably with independent power and control paths | Redundant lift motors plus independent cruise propulsion | The aircraft should maintain controlled flight or execute a safe landing after a single propulsion fault where the design permits. |
| Energy Storage | High-voltage lithium battery packs with battery-management systems | Multiple isolated battery packs with cell-temperature and voltage monitoring | Battery-electric lift system with battery, fuel, or hybrid-electric cruise system | Check usable energy rather than nominal capacity, and include a reserve for unexpected wind or diversion. |
| Navigation Sensors | Multi-constellation GNSS, inertial measurement unit, barometer, magnetometer | Dual GNSS or GNSS with inertial navigation, radar or laser altimeter, terrain awareness | Dual GNSS, inertial navigation, air-data sensors, barometer, and terrain or radar altitude sensing | A suitable system should continue stable navigation during temporary GNSS degradation or short signal interruptions. |
| Positioning Accuracy | Approximately 1–3 m with standard satellite positioning; centimeter-level with correction services | Approximately 1–3 m with standard satellite positioning; centimeter-level with correction services | Approximately 1–3 m with standard satellite positioning; centimeter-level with correction services | Use corrected positioning only when the operating area has reliable correction coverage and an independent fallback. |
| Obstacle Detection | Forward, downward, and side-facing cameras or lidar | 360-degree sensing using lidar, radar, cameras, or a combined sensor set | Forward radar or lidar, terrain sensing, and landing-zone detection | Sensor coverage should match the aircraft's speed, stopping distance, rotor span, and operating environment. |
| Terrain and Landing Assistance | Downward optical flow, lidar, or radar altimeter | Radar or lidar altimeter with landing-zone assessment | Radar altimeter, terrain database, and automated approach or landing guidance | For uneven or unprepared sites, prioritize accurate low-altitude sensing and landing-zone verification. |
| Control Architecture | Redundant flight controller with stabilized manual, assisted, and automatic modes | Dual flight computers, monitored actuator outputs, and independent emergency logic | Separate flight-control functions for VTOL, transition, cruise, and return-to-home operations | Control software should provide clear mode status, fault alerts, geofencing, and operator override. |
| Communication Link | Encrypted command and telemetry link with cellular or radio backup | Redundant long-range links with automatic link-quality monitoring | Long-range command link with cellular, satellite, or radio redundancy where permitted | Design the link budget for terrain, antenna placement, interference, and the maximum legal operating distance. |
| Loss-of-Link Response | Return to home, hover, land, or proceed to a predefined safe point | Return, controlled holding pattern, or alternate landing site with cargo-release lockout | Route continuation, diversion, loiter, or automated landing based on the current flight phase | The response must be configurable, predictable, and tested under realistic communication-loss conditions. |
| Power-Failure Protection | Battery health monitoring, low-voltage warning, and reserve-energy landing logic | Independent battery packs, thermal monitoring, and automatic emergency landing procedures | Separate energy management for lift and cruise systems with controlled transition or landing modes | Require automatic warnings before reserve energy is reached and prevent launch when battery condition is unsafe. |
| Cargo Safety | Mechanical restraint, door sensor, and payload-presence verification | Positive locking mechanism, load monitoring, and emergency cargo-release prevention | Locked cargo bay, door-status monitoring, and center-of-gravity limits | Cargo must remain secured during acceleration, turbulence, landing impact, and emergency maneuvers. |
| Weather Capability | Light rain and moderate wind only when permitted by the approved operating limits | Weather-resistant components with strict limits for wind, precipitation, icing, and visibility | Higher cruise-wind tolerance but greater sensitivity to icing, turbulence, and runway or landing-site conditions | Never infer weather capability from appearance; use documented limits and current site weather data. |
| Wind Tolerance | Commonly about 8–12 m/s, depending on payload and airframe | Commonly about 8–12 m/s, with reduced endurance at higher wind speeds | Often better in cruise, but VTOL takeoff and landing may remain limited to approximately 8–12 m/s | Evaluate gusts, crosswinds, wind direction, and the effect of wind on return-flight energy reserves. |
| Operational Safety Features | Geofencing, remote identification where required, strobe lighting, propeller guards, and emergency stop logic | Geofencing, remote identification where required, conspicuity lighting, redundant controllers, and emergency landing management | Geofencing, remote identification where required, aviation lighting, flight-phase protection, and terrain-aware diversion logic | Verify that safety functions are documented, independently tested, and compatible with local aviation requirements. |
| Maintenance Requirements | Frequent inspection of motors, propellers, batteries, arms, and landing gear | Detailed inspection of propulsion units, structural joints, cargo restraints, batteries, and cooling systems | Inspection of lift motors, cruise propulsion, wings, control surfaces, transition mechanisms, and energy systems | Choose a platform with documented inspection intervals, accessible components, diagnostic logs, and replaceable parts. |
| Best-Fit Mission | Short-range delivery, construction sites, farms, and precise point-to-point lifting | Heavy loads over short distances where hover precision and vertical access are essential | Long-distance logistics, remote-area supply, medical transport, and routes with limited road access | Match the aircraft to route length, cargo mass, takeoff and landing conditions, and required delivery accuracy. |