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Volitation Innovations TX-60V

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

The Volitation Innovations TX-60V is a hybrid-wing/fixed-wing flight platform supplied as an airframe and propulsion package. It combines lightweight, structurally load-bearing motor arms with a large payload compartment for mission integration. Maximum takeoff weight is 60 kg; its 22 kg load capacity includes fuel.

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Supplied configurationAirframe and propulsion package in the hybrid-wing/fixed-wing category.
Maximum takeoff weight60 kg
Load capacity22 kgIncludes fuel.
Arm architectureLightweight arms serve as vertical-lift motor mounting members and form a closed load-bearing structure that increases resistance to bending and torsion.
Payload compartmentLarge payload compartment intended to support multiple mission configurations, convenient maintenance and rapid deployment.

Product overview

The Volitation Innovations TX-60V is a flight platform offered as an airframe and propulsion package within the hybrid-wing/fixed-wing category. Its stated maximum takeoff weight is 60 kg, with a load capacity of 22 kg including fuel. That qualification matters for mission planning: the 22 kg figure covers fuel as well as the carried load, so it cannot be treated as a dedicated equipment allowance independently of the fuel carried.

The physical architecture combines lightweight arms with a large payload compartment. The arms provide mounting members for the vertical-lift motors while also forming a closed load-bearing structure designed to improve resistance to bending and torsion. The compartment provides integration space for different mission configurations, with an emphasis on maintenance access and rapid deployment. The supplied configuration is identified as an airframe and propulsion package, which defines the procurement scope more specifically than the flight-platform designation alone.

Specifications

SpecificationValue & conditions
Supplied configurationAirframe and propulsion package in the hybrid-wing/fixed-wing category.
Maximum takeoff weight60 kg
Load capacity22 kgIncludes fuel.
Arm architectureLightweight arms serve as vertical-lift motor mounting members and form a closed load-bearing structure that increases resistance to bending and torsion.
Payload compartmentLarge payload compartment intended to support multiple mission configurations, convenient maintenance and rapid deployment.
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