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3D-Printed Tethered Drone Fuselage: Military-Grade Structural Components Pass Full MIL-STD-810H Qualification

CRP USA collaborated with Hoverfly Technologies to manufacture end-use structural components for fielded TeUAS platforms. The project highlights how additive manufacturing enables functional integration, design freedom, and structural reliability in operational systems.

DEFENSE CASE STUDY
In Short
Challenge
Manufacture lightweight, high-strength structural parts with complex internal geometries for cable routing and optimized load paths, not achievable at the required speed/complexity with traditional manufacturing
Technology
SLS
Material
Windform GT
Result
Fuselages passed full MIL-STD-810H qualification, ensuring structural integrity, reduced weight, functional integration, and reliable operation in harsh environments
Gallery
Underside view of Hoverfly’s Spectre 2.0 drone during tethered flight, showing the central section and suspension system
Underside view of Hoverfly’s Spectre 2.0 drone during tethered flight, showing the central section and suspension system

End-Use components for TeUAS platforms

Hoverfly Technologies, leader in tethered drone solutions, partnered with CRP USA to manufacture the main fuselage for its Spectre 2.0 and Sentry platforms. The result was 3D-printed, end-use production parts, not prototyping or testing only, used on fielded systems. Designed by Hoverfly engineers and manufactured by CRP USA for long-term integration, not routine replacement.

The collaboration with CRP USA enabled Hoverfly to develop highly specialized TeUAS platforms capable of operating in demanding military, security, and tactical missions, with structural solutions fully supporting multi-payload configurations, persistent ISR, advanced electronic warfare, and network extension roles.

Focus

A TeUAS (Tethered Uncrewed Aerial System) is a drone platform connected to a ground station via a power and data tether, enabling continuous flight, persistent surveillance, and secure real-time data transmission.

Complex geometries and rapid deployment needs

Hoverfly required lightweight, high-strength structural parts featuring complex internal geometries for embedded cable routing and optimized load paths. There requirements were combined with rapid production timelines for operational deployment and the ability to perform reliably in harsh environments: vibrations, temperature extremes (-20°C to +49°C), rain, dust, mechanical shocks.

Front view of Hoverfly’s Spectre 2.0 drone in operational configuration, showing the structure and arms in flight layout
Front view of Hoverfly’s Spectre 2.0 drone in operational configuration, showing the structure and arms in flight layout

Traditional manufacturing methods such as CNC machining and injection molding, could not meet these requirements.

3D Printing solution: material and process

Selective Laser Sintering (SLS) with glass fiber reinforced thermoplastic Windform GT enabled:

  • Load-bearing structures with thin-wall designs
  • Weight optimization without compromising strength
  • Complex internal geometries impossible with conventional methods
  • Fast production cycles meeting tight deployment timelines
  • Full airframe integrity connecting booms and housing electronic components
Front view of Hoverfly’s Sentry drone equipped with an operational payload, with the sensor mounted beneath the platform
Front view of Hoverfly’s Sentry drone equipped with an operational payload, with the sensor mounted beneath the platform

Key engineering benefits

Function Integration

Structural, mounting and housing functions integrated

Reduced Part Count

Simplified BOM, fewer components to manage

Design Freedom

Complex routing, embedded channels, load paths

Faster Development

Accelerated iterations, quick cycles, shorter lead time

Lightweight and mechanical strength

Thin-wall sections ensuring strength and durability

MIL-STD Qualified

Validated performance under military standards

Military-grade qualification

All Windform GT components passed full MIL-STD-810H environmental testing.

Test
Reference
Drop testing
MIL-STD-810H-C1, Method 516.8
Temperature cycling (-20°C to +49°C)
MIL-STD-810H-C1, Methods 501.7 / 502.7
Blowing rain and wind
MIL-STD-810H-C1, Method 506.5
Blowing dust (6h exposure, 49°C)
MIL-STD-810H-C1, Method 510.7
Continuous flight
48-hour operational test

All parts maintained full functional and structural integrity throughout.

Results achieved

The 3D-printed Windform GT fuselage structures proved structurally reliable and operationally robust in demanding mission conditions. The components ensured safe flight performance, optimized endurance through lightweight design, and reliable operation under harsh environments, while reducing part count and enabling modular system configurations.

Looking Ahead

Following the success of this collaboration, Hoverfly is actively exploring further additive manufacturing applications, including embedded EMI shielding, integrated thermal management, and smart structures for future TeUAS generations.

"Additive manufacturing, especially with Windform composites, was a critical enabler for our rapid development timelines and complex drone structures. It eliminated trade-offs between performance and production agility."
Jeff Van Anda, SVP Engineering, Hoverfly Technologies
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