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COMMERCIAL AIRCRAFT

Volitation Innovations TX-30V

By Volitation Innovations (Beijing) Science & Technology Co., Ltd. ↗

The Volitation Innovations TX-30V is a modular compound-wing/fixed-wing UAV airframe and propulsion package with a 30 kg maximum takeoff weight. Endurance is 2 h with a 10 kg payload or 4 h with 4 kg. Its two-section fuselage and integrated tail/rear landing gear support smaller packed volume and tool-free deployment and pack-down.

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Maximum takeoff weight30 kg
Endurance2 hWith a 10 kg payload.
Supplied configurationCompound-wing/fixed-wing UAV airframe and propulsion package.
Endurance4 hWith a 4 kg payload.
Modular constructionHighly modular structure with quick disassembly.
Tool requirementsNo tools required.During deployment and pack-down.

Product overview

The Volitation Innovations TX-30V from Volitation Innovations (Beijing) Science & Technology Co., Ltd. is a long-endurance UAV supplied as an airframe and propulsion package in the compound-wing/fixed-wing category. It has a maximum takeoff weight of 30 kg. Its endurance figures are tied to carried payload: 2 h with 10 kg and 4 h with 4 kg. Those payload conditions are integral to the respective endurance ratings.

The physical architecture uses a two-section fuselage and combines the tail assembly with the rear landing gear. This integrated arrangement simplifies the system composition and reduces packed volume. The structure is highly modular and designed for quick disassembly, with no tools required for deployment or pack-down. The propulsion package uses strictly screened component selection and optimized design, complementing the airframe’s emphasis on integration, modular construction and compact packing.

Specifications

SpecificationValue & conditions
Supplied configurationCompound-wing/fixed-wing UAV airframe and propulsion package.
Maximum takeoff weight30 kg
Endurance2 hWith a 10 kg payload.
Endurance4 hWith a 4 kg payload.
Modular constructionHighly modular structure with quick disassembly.
Tool requirementsNo tools required.During deployment and pack-down.
Tail and rear landing gearTail assembly and rear landing gear combined into one structure.
Fuselage constructionTwo-section fuselage.
Integrated architectureSimpler system composition and smaller packed volume.
Propulsion selection and designStrictly screened propulsion selection and optimized design.
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