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COMMERCIAL AIRCRAFT

V2000CG

By AutoFlight ↗

The Autoflight V2000CG CarryAll is a ton-class, all-electric unmanned cargo eVTOL combining vertical take-off and landing with fixed-wing cruise. Its standard configuration provides a maximum payload of 400 kg, up to 3.2 m³ of cargo volume and an operational range of 200 km.

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Autoflight V2000CG CarryAll aircraft flying above the coast.
Autoflight V2000CG CarryAll aircraft flying above the coast.
Maximum payload400 kg.Standard configuration.
Maximum take-off weight2000 kg.Standard configuration.
Product and purposeAutoflight V2000CG CarryAll; ton-class unmanned cargo eVTOL for aerial logistics.
Flight architectureVertical take-off and landing with fixed-wing cruise.
Aircraft dimensionsWingspan 15 m × length 11.6 m × height 3.3 m.Standard configuration.
Propulsion typeAll-electric.Standard configuration.

Product overview

The Autoflight V2000CG CarryAll is an unmanned cargo aircraft for medium-to-long-distance aerial logistics. Its flight architecture combines vertical take-off and landing with fixed-wing cruise, allowing runway-free transport operations. The standard configuration uses all-electric propulsion and measures 15 m in wingspan, 11.6 m in length and 3.3 m in height. It has a maximum take-off weight of 2000 kg, a maximum payload of 400 kg and a maximum cargo volume of 3.2 m³.

Cargo accommodation is defined by both the payload ceiling and available volume. The standard configuration has an operational range of 200 km and a maximum operating altitude of 3000 m. Its distributed propulsion architecture gives each propulsion unit independent dual power supplies and dual communication interfaces. Four mutually independent battery packs support the electrical architecture, with multi-level battery management and real-time condition monitoring. The V2000CG has completed full civil aviation airworthiness certification.

Specifications

SpecificationValue & conditions
Product and purposeAutoflight V2000CG CarryAll; ton-class unmanned cargo eVTOL for aerial logistics.
Flight architectureVertical take-off and landing with fixed-wing cruise.
Aircraft dimensionsWingspan 15 m × length 11.6 m × height 3.3 m.Standard configuration.
Propulsion typeAll-electric.Standard configuration.
Maximum take-off weight2000 kg.Standard configuration.
Maximum payload400 kg.Standard configuration.
Maximum cargo volume3.2 m³.Standard configuration.
Operational range200 km.Standard configuration.
Maximum operating altitude3000 m.Standard configuration.
Distributed propulsion architectureAeronautical-grade cross-redundant architecture; each propulsion unit has independent dual power supplies and dual communication interfaces.
Battery architecture and managementFour mutually independent battery packs, with thermal management, protection and energy safety design, multi-level battery management and real-time condition monitoring.
Airworthiness certificationCompleted full civil aviation airworthiness certification.
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