Mission positioning
A remote last-mile feeder for the national nutrition network—not a replacement for bulk road distribution. Trucks retain high-volume trunk routes while DA6200-XR serves remote, island, highland or time-sensitive spokes.
A hydrogen fuel-cell or generator-hybrid aircraft for scheduled delivery from SPPG kitchens to remote schools, islands, highlands and traffic-constrained communities.
DA6200-XR combines vertical take-off, protected distributed propulsion and efficient wing-borne cruise with an interchangeable hydrogen fuel-cell or generator-hybrid energy module and an enlarged sealed MealPod.
A remote last-mile feeder for the national nutrition network—not a replacement for bulk road distribution. Trucks retain high-volume trunk routes while DA6200-XR serves remote, island, highland or time-sensitive spokes.
Hydrogen and generator-hybrid configurations are separate engineering targets. All values require detailed design, safety analysis, prototype testing and Indonesian regulatory approval.
Each participating SPPG restaurant or central kitchen provides 3,000 meals per day. DA6200-XR is positioned as a remote last-mile feeder for selected schools rather than a replacement for bulk road distribution. A starter pilot cell uses two operating aircraft plus one reserve, an approved energy station, one RTK / weather station and two controlled MealPorts.
SPPG packs meals, checks temperature, seals the MealPod and scans the manifest.
MealPod locks into the aircraft; weather, route and reserve energy are verified.
Supervised route with geofence, reserve-energy logic and live telemetry.
Land at a controlled MealPort; authorized staff scan and receive the shipment.
Aircraft returns, packs swap, logs upload and the MealPod is sanitized.
The 3,000-meal figure is the daily output of each restaurant / SPPG kitchen. The aircraft fleet does not need to carry all 3,000 meals unless the selected route plan assigns the full kitchen output to aerial delivery; road vehicles can continue to serve bulk routes.
Target MTOW is 115 kg for the hydrogen configuration and 118 kg for the generator-hybrid configuration. Both are outside Indonesia’s small-UAS category of no more than 25 kg, so the airworthiness and operating pathway must be confirmed with the Directorate General of Civil Aviation before prototype flight or service.
Select SPPG-school corridors, map people, roads and airspace, verify spectrum and define emergency sites.
Freeze loads, propulsion, H₂ or fuel containment, software assurance, interfaces and FMEA.
Validate structure, energy module, leak / fire detection, EMI / EMC, parachute, MealPod and thermal hold.
Confirm the Part 22 airworthiness and operating-approval pathway, registration and operator requirements.
Progress from a closed test area to a representative route, including lost-link and contingency demonstrations.
Approve tray geometry, loading SOP, hot / cold time-temperature envelope, cleaning and chain of custody.
Operate limited routes with observers, school safety zones, daily review, incident reporting and independent audit.
Use verified cost, reliability, safety and food-quality data to decide fleet size and additional SPPG locations.
Final values remain subject to detailed engineering, hydrogen or fuel-system safety analysis, thermal validation, prototype testing, food-safety validation and Indonesian regulatory approval.
Open Complete SpecificationDAES AI PTE LTD · Singapore | Taiwan | Indonesia