Industry Aerospace
Aerospace

Propelling the field of small sats forward with PBF 3D printing and Windform® XT 2.0 Carbon fiber filled composite material

Using professional 3D printing and Carbon fiber filled Windform XT 2.0 composite material, CRP Technology manufactured OGMS-SA, a 3U technological CubeSat structure. It is a demonstrator flight-ready in low earth orbit, with 2 deployed solar panels connected to a power supply distribution to control the batteries and to provide the power buses to the satellite.

3D printed 3U CubeSat structure via laser sintering technology using Windform© XT 2.0
In Short

Application

3U technological demonstrator Cubesat

Solution

Selective Laser Sintering and Windform® XT 2.0 Carbon fiber filled composite material

Challenge

Manufacturing a 3U CubeSat formfactor that withstands the design and launch-pad requirements in terms of dimension, flatness and roughness, mass optimization, internal parts integration, but also for outgassing, UV resistance, thermal expansion, and overall space constraint.

Features of the application

Field tested required
Fulfillment outgassing criteria
Functional component
High mechanical performances
Lightweight
Resistant to thermal vacuum test
Space/flight ready

Customer's requests

Highly customizable
Maintaining high-end user quality standards
Minimized production speed
No tooling cost
Reduced time to market
Remarkable accuracy

Services supplied

Complete engineering assistance
Suggestions for overcoming critical application consultancy
Technology and material selection
Testing

3D printed 3U CubeSat structure via laser sintering technology using Windform© XT 2.0
3D printed 3U CubeSat structure via laser sintering technology using Windform© XT 2.0

Space industry has been revolutionized by the ever-increasing production and launch of small satellites.

Additive manufacturing technologies not only helped this radical change to be fulfilled, but have itself reached new heights with the manufacture of structural components for the new generation of Space parts using high performance composite materials.
Although much still must be done to reach an extensive use of additive manufacturing for Space applications, CRP Technology’s built a considerable experience supplying cutting-edge solutions for space key industry leaders. A clear and remarkable example comes from the experience with LISA.

The Italian-based company specialist for over 25 years in the use and development of advanced additive manufacturing technologies and materials, collaborated with the Laboratoire InterUniversitaire des Système Atmosphérique (LISA) of Universite Paris-est Creteil (UPEC) on the construction of a nano-satellite that is a 3U CubeSat formfactor.
The project was carried by students under CNES and Space Campus University supervision.

The goal was to develop a demonstrator that can be flight-ready in Low Earth Orbit.
The engineering team at LISA and CNES decided to rely on CRP Technology and its Windform® TOP-LINE family of high performance materials for the manufacturing of the nano-satellite.

The project manager at LISA, commented, “Using such a process and composite material from Windform’s® TOP-LINE, we knew for sure we would be able to design the structure exactly the way we needed it.”
The structure had to survive vibration tests (to endure the launch) and thermal-vacuum tests. It had also to withstand outgassing requirements.

Left: Mechanical solar panel deployment frame integrated in the 3D printed structure. Right: Battery Cradle integrated in the 3D printed structure – courtesy of LISA
Left: Mechanical solar panel deployment frame integrated in the 3D printed structure. Right: Battery Cradle integrated in the 3D printed structure – courtesy of LISA

“The design has been done taking into account all of these constraints – the project manager at LISA added – . CRP Technology’s support was crucial to achieve our aims. Their Windform® TOP-LINE materials and additive manufacturing/Powder Bed Fusion process with composite polymers fibers-reinforced allowed us to reduce mass and optimize the way to integrate parts inside the CubeSat.

CubeSat Structure is critical as it has to fulfill the launch-pad (P-Pod) requirements in terms of dimension, flatness and roughness, but also for outgassing, UV resistance, thermal expansion, and general space constraints.
Plus, if it breaks, or stays stuck in the P-pod launcher, the mission is over.

The assignment was tough, but thanks to the long-term experience gained in the field of additive manufacturing service alongside the key leaders of the most advanced industrial sectors CRP Technology accepted the challenge.
The activity of CRP Technology’s 3D Printing department has been focused from the beginning on maximizing and achieving the targets required, providing full collaboration to the team at LISA.

Work began with an accurate analysis of the 3D and 2D files: through their long-standing technological expertise, CRP Technology suggested alterations that made it possible to optimize the geometries of the parts, reaching the required target in terms of mass optimization and part integration.

3U-CubeSat OGMS-SA (OutGassing Material Study by Spectroscopy Analysis) with solar panels and antennas deployed – courtesy of LISA
3U-CubeSat OGMS-SA (OutGassing Material Study by Spectroscopy Analysis) with solar panels and antennas deployed – courtesy of LISA

Through the know-how earned in over 25 years of activity serving the most demanding and high-performance industrial sectors, CRP Technology has been able to assist LISA and CNES in choosing the best technology and material to guarantee the success of the project: PBF selective laser sintering and Windform® XT 2.0 Carbon composite material.

Windform® XT 2.0 replaces the previous formula of Windform® XT in the Windform® TOP-LINE family of composite materials.
Windform® XT 2.0 features improvements in mechanical properties including +8% increase in tensile strength, +22% in tensile modulus, and a +46% increase in elongation at break. These mechanical properties have guaranteed the achievement of the required characteristics, i.e. stiffness, low mass as well as very smooth surface finish.

Once received the .STP file with optimized geometries from LISA, CRP Technology created in a short time the functional 3D printed component (the nano-satellite structure) via selective laser sintering using Windform® XT 2.0.

PBF Professional 3D printing, combined with Windform® XT 2.0 Carbon-composite material, proved to be the best choice: the 3D printed part has successfully passed the control and testing criteria, and has fully complied with the requests and LISA’s standards.

LISA and CNES performed many tests on the 3d printed nano-satellite structure such as vibration tests and thermal-vacuum tests. They were very satisfied with the results obtained.

Thanks to CRP’s laser sintering technology and Windform® XT 2.0 Carbon-reinforced composite material, we obtained very important key advantages such as mass reduction, component integration, outgassing control, thermal expansion, and low surface roughness. We are more than satisfied with selective laser sintering technique Powder Bed Fusion process and consider Windform® XT 2.0 one of the disruptive revolutions in the small satellites arena. We do hope to use additive manufacturing intensively in space application
LISA team