Product overview
The Volitation Innovations TX-100V (TW), from Volitation Innovations (Beijing) Science & Technology Co., Ltd., is a payload-carrying flight platform supplied as an airframe and propulsion package in the compound-wing/fixed-wing category. Its maximum takeoff weight is 100 kg, with endurance of 4.4 hours when carrying a 30 kg payload. The endurance figure therefore applies to that payload configuration. Its physical architecture combines vertical-lift arms, forward and rear wings, and a fuselage, with an integrated vertical tail and landing gear arrangement.
Aviation carbon-fiber composite forms the platform’s structure, and the vertical-lift arms use integral prepreg molding. These arms connect with the forward wing, rear wing and fuselage to create a closed load-bearing structure that increases resistance to bending and torsion. The integrated tail and landing gear design simplifies the structure and improves aerodynamic and energy efficiency. Control redundancy uses two forward and four rear control surfaces, with single and dual control-surface fault tolerance, diagonal failure capability, opposing-surface linked actuation and coordinated control.
Specifications
| Specification | Value & conditions |
|---|---|
| Manufacturer and model | Volitation Innovations (Beijing) Science & Technology Co., Ltd.; Volitation Innovations TX-100V (TW) |
| Supplied configuration | Compound-wing/fixed-wing flight platform supplied as an airframe and propulsion package.Airframe and propulsion package. |
| Maximum takeoff weight | 100 kg |
| Endurance | 4.4 hWith a 30 kg payload. |
| Tail and landing gear architecture | Integrated vertical tail and landing gear design that simplifies the structure and improves aerodynamic and energy efficiency. |
| Structural material | Aviation carbon-fiber composite. |
| Vertical-lift arm construction | Vertical-lift arms manufactured using an integral prepreg molding process. |
| Load-bearing structure | The vertical-lift arms, forward wing, rear wing and fuselage form a closed load-bearing structure that strengthens resistance to bending and torsion. |
| Control-surface arrangement | Redundant arrangement with two forward and four rear control surfaces. |
| Control-surface fault tolerance | Single and dual control-surface fault tolerance.Single or dual control-surface failures. |
| Control capabilities | Supports diagonal failure scenarios, opposing-surface linked actuation and coordinated control. |
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