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X4-1900H Hydrogen Fuel Cell Drone for Heavy Payload Delivery

Price: $
Model: X4-1900H equipment envelope
Wheelbase: Archived: 1900mm X8 frame
Flight Control: Propulsion and fuel-cell control revision — confirm
Empty Weight: Archived: 18m/s — define acceptance profile
Power Battery: Archived: two 6S 5300mAh auxiliary packs
Wingspan(without propellers): Archived unfolded: 1500 × 1500 × 650 mm
Folded Size(without propellers): Archived folded: 900 × 800 × 650 mm
Empty Weight: Conflict: 14.5kg vs 16kg empty mass
Satellite Navigation System: Multi-GNSS and RTK option — identify equipment
Endurance Time: Two-hour no-load entry is not installed-equipment time
Maximum Horizontal Speed: Archived: 18m/s — define acceptance profile
Image Transmission: Link equipment remains to be identified
Electronic Speed Controller: Archived fuel-cell output: 48V, 3kW

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Identity not releasedEquipment-carrying envelope

Calculate the remaining allowance from a weighed delivered aircraft

The archived title uses sensitive payload language, so this record stays on a civil-use identity hold. It may support lawful industrial carrying or inspection discussions only after payload interface, mass, permissions and acceptance evidence are defined. The X4-1900H source names an X8 propulsion set, 1900mm frame, 14.5kg empty-weight figure and 29kg maximum take-off entry at a stated throttle point. An older product field says 16kg empty. The page title refers to heavy payload delivery, but subtraction of disputed archive values would not establish a safe equipment allowance. For lawful inspection, survey or logistics support, begin with calibrated mass, mounting limits and a manufacturer-approved envelope.

Reasons for the identity pause

  • Open 1Weight conflict: 14.5kg body entry versus 16kg old field.
  • Open 2Interface evidence: document mount, fasteners, wiring, power and balance.
  • Open 3Acceptance evidence: test the exact installed civil equipment with reserve.

Mass-envelope calculation inputs

InputArchived entryRequired current value
Empty mass14.5kg in body; 16kg in old fieldCalibrated aircraft with defined included items
Maximum take-off29kg at a stated throttle pointApproved revision-specific limit and basis
Energy equipmentFuel cell, cylinder and two auxiliary packsFilled condition and installation mass
Civil equipmentCamera, scanner or other lawful loadMass, mount, power, balance and test
Top-down photograph of a black folding aircraft with its arms folded beside a glossy central body.
Identity reference only; the image does not verify a payload mount, installed mass, balance or permitted use.

Evidence for an installed civil load

  1. Resolve the 14.5kg/16kg empty-weight discrepancy.
  2. Obtain the airframe revision and approved mass envelope.
  3. Weigh aircraft, energy system, mount and equipment separately.
  4. Confirm interface drawing, fasteners, power and centre of gravity.
  5. Run a controlled acceptance profile with agreed reserve.

Include mounting hardware and cables in the total

Useful equipment is not only the sensor or parcel. Brackets, vibration isolation, wiring, protective enclosure and attachment hardware all consume mass and can shift the centre of gravity.

Separate transport planning from aircraft performance

Ground packaging, cylinder rules, site handling and loading procedures determine whether the system can be deployed. The flight acceptance file should focus on the approved installation, mass, balance, energy state, reserve and controlled result.

Equipment-envelope questions

Is 29kg minus 14.5kg the usable payload?
No. Included items, weight conflict, structure, centre of gravity and operating reserve remain unresolved.
What belongs in the installed equipment weight?
Include mount, fasteners, wiring, enclosure, sensor and any dedicated power hardware.
Why weigh the energy system separately?
Cylinder fill state and auxiliary batteries affect total mass and repeatability.
Request a current equipment envelope

Send the lawful equipment mass and interface needs for a revision-specific review.

Compare large industrial platforms
Identity Hold

Civil payload identity hold

Remove operational delivery implications from the commercial product record.

01
Limit discussion to lawful industrial carrying, inspection or sensor integration.
02
Document payload mass, attachment, centre of gravity and permitted use.
03
Require configuration and acceptance evidence before releasing capability wording.

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Customer Reviews

   

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   Long Transmission and Good Build Quality


 2025-12-30

The long-distance capabilities of this drone impressed me right away. It kept a reliable link out to several kilometers, and the sturdy build handled a few rough landings without issue. A solid choice for expansive FPV flights
   Extended Flight Range, Smooth Controls


 2025-12-30

Using this drone for scenic long-range flights has been an amazing experience. Controls feel smooth even at the edge of transmission range, and the battery life lets me stay airborne for extended sessions. Ideal for explorers and aerial photographers alike
   Great Balance of Range and Stability


 2025-12-30

My experience with the FPV Drone has been positive overall. The long-range capability is solid for cruising and exploration flights, and the stable flight characteristics in crosswinds give me confidence flying farther out. Perfect for intermediate pilots looking to push their limits
   Awesome Long Range FPV Footage


 2025-12-30

I mounted a lightweight camera on my Long Range FPV and got stunning FPV footage over open fields and trails. The signal stayed strong over long distances, and the build held up well to minor bumps. Definitely a great rig for scenic long flights
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