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Every gram counts: optimizing mass and performance in Aerospace with Roboze superpolymers

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Context: lightweight engineering as a design lever

In the aerospace industry, the mass of each component represents a critical design variable.
Even a modest reduction, on the order of 1 kg, can generate fuel savings and increased payload capacity, with immediate economic impact.

According to NASA estimates published in  “The Recent Large Reduction in Space Launch Cost”, launching payloads to LEO (Low Earth Orbit) with a Falcon 9 costs approximately USD 2,720 per kilogram, based on a 22,800 kg mission valued at USD 62 million. For a 500 kg satellite, reducing just 1 kg of mass translates into a saving of roughly USD 2,700, along with gains in autonomy and payload efficiency.

In this context, additive manufacturing with Roboze superpolymers emerges as an industrial solution for reducing weight, simplifying assemblies, and improving sustainability.
Materials such as Carbon PEEK and ULTEM™ AM9085F, processed on the ARGO 500 HYPERSPEED platform, enable the production of integrated, lightweight structures, eliminating the geometric constraints and fasteners typical of metal manufacturing processes.

 

3D sandwich structures: a case of applied engineering

A tangible example of this transition comes from the University of Campania “Luigi Vanvitelli”, in collaboration with Roboze, which developed 3D-printed aerospace sandwich structures using the ARGO 500 HYPERSPEED platform.

The goal was to replace traditional metallic panels with a monolithic Carbon PEEK structure, integrating skins and honeycomb core in a single process.
The use of a polymer matrix composite combined with the elimination of adhesives and mechanical joints achieved a 52% mass reduction while maintaining stiffness comparable to metal, stable above 200 °C.

Roboze Carbon PEEK: material properties and system performance

The results of the Vanvitelli–Roboze case study are consistent with the official Roboze Carbon PEEK datasheet (available for download).

To assess its real impact, it is essential to distinguish between material properties and printed component performance.

A) Material property comparison

Parameter

Al Alloy 7075-T6

Roboze Carbon PEEK

Δ Variation

Source

Density [g/cm³]

2.81

1.41

−50 %

MatWeb 7075-T6 / Roboze TDS

Flexural Modulus [GPa]

70–72

9.74

−86 %

ASTM D790 – Roboze TDS

Flexural Strength [MPa]

≈ 550 (base material)

124.6 (XZ)

−77 %

ASTM D790 – Roboze TDS

Outgassing (XZ)

TML 0.190 % / CVCM 0.002 %

Roboze White Paper

 

B) Structural performance – printed sandwich panel

Parameter (panel)

Al 7075-T6 (traditional)

Roboze Carbon PEEK

Δ Variation

Source

Panel Mass [g] (300×300 mm)

510

255

−50 %

Proportional calculation

Flexural Performance (component)

~68

~61

−10 %

doi: 10.1016/j.ast.2023.108276

Operating Temperature [°C]

180

250

+39 %

Roboze TDS / White Paper

Design Notes

Metallic structure

Integrated honeycomb core → ↑ inertia / ↓ joints

FEA + Vanvitelli tests

 

Numerical analysis and interpretation

Roboze Carbon PEEK, tested in XZ orientation per ASTM D790, shows a flexural strength of 124.6 MPa and modulus of 9.74 GPa, values that describe the real behavior of a 3D-printed component, including interlayer response.

Although lower than metals in absolute terms, these values, combined with half the density (1.41 g/cm³) and thermal stability beyond 250 °C, yield an exceptionally high strength-to-weight ratio, enabling the substitution of aluminum in many secondary aerospace structures.

Roboze’s technology, through topological optimization and geometric continuity, maintains global stiffness and strength while reducing overall component mass by up to 50% and assembly costs by 30%, delivering tangible gains in production efficiency and sustainability.

 

Economic simulation: the value of weight reduction

Parameter

Estimated Value

Description

Total mass (Al alloy)

30 kg

baseline configuration

Total mass (Carbon PEEK)

15 kg

−50 % mass

Weight saved

15 kg

difference between systems

Launch cost avoided

≈ USD 40,500

15 kg × 2,700 USD/kg (NASA report)

Assembly cost reduction

−30 %

joint elimination

Production time

−40 %

print-to-part < 48 h (ARGO 500 HS)

Estimated operational ROI

+25–30 %

mission lifecycle

 

Each kilogram saved in orbit represents about USD 2,700 in direct savings, plus additional logistical and manufacturing benefits.
Roboze additive manufacturing converts weight reduction into a quantifiable economic advantage, enhancing efficiency and sustainability throughout the mission lifecycle.                

 

Roboze Carbon PEEK: composite material for extreme performance

Tested according to ASTM E595 and ESA ECSS-Q-ST-70-02C, Roboze Carbon PEEK demonstrates exceptionally low outgassing performance.

Property

Standard

XZ Orientation

NASA Limit

Total Mass Loss (TML)

ASTM E595

0.190 %

≤ 1 %

Collected Volatile Condensable Material (CVCM)

ASTM E595

0.002 %

≤ 0.1 %

Recovered Mass Loss (RML)

ASTM E595

0.076 %

 

Source: Roboze White Paper – “Outgassing Behavior of Carbon PEEK” (ARGO 500 HYPERSPEED).

Values two orders of magnitude below NASA limits confirm compatibility with optical payloads, satellite structures, and avionic components.

Engineering advantages:

  • Thermal stability beyond 250 °C

  • Specific strength > 120 MPa·cm³/g

  • Vacuum-grade compatibility without coatings

  • Reduced anisotropy through orientation control

  • Excellent chemical and dimensional stability

 

ULTEM™ AM9085F: the certified aerospace solution

ULTEM™ AM9085F, a high-performance amorphous thermoplastic (PEI-based), combines lightweight, rigidity, and thermal stability up to 175 °C.
It is certified for aerospace use through FAA FAR 25.853 and OSU 55/55 tests, confirming its FST (Flame, Smoke, Toxicity) compliance.
The full datasheet is available on the Roboze ULTEM™ AM9085F page.

Property

Average Value

Standard

Tensile Strength (XZ)

89 MPa

ASTM D638

Elastic Modulus

2.5 GPa

ASTM D638

HDT (1.82 MPa)

175 °C

ASTM D648

Density

1.27 g/cm³

ASTM D792

Compressive Strength

93–98 MPa

ASTM D695

 

ULTEM™ AM9085F is ideal for brackets, ducts, electronic housings, and interior aircraft components in pressurized cabins, due to its dielectric stability and chemical resistance in demanding environments.

Comparative table: Roboze materials for aerospace

Key Property

Roboze Carbon PEEK

ULTEM™ AM9085F

HDT (XZ)

245 °C

175 °C

Density

1.50 g/cm³

1.27 g/cm³

Outgassing (TML/CVCM)

0.19 % / 0.002 %

N/A

Tensile Strength (XZ)

146 MPa

89 MPa

Elastic Modulus (XZ)

10.1 GPa

2.5 GPa

Thermal Conductivity

0.9 W/m·K

0.21 W/m·K

Typical Applications

Satellite structures, optical payloads, vacuum chambers

Ducts, interior panels, avionics brackets

 

Conclusion: structural efficiency and competitive advantage

Thanks to Roboze superpolymers and the ARGO 500 HYPERSPEED platform, the aerospace industry can now combine weight reduction, high mechanical performance, and environmental compliance with the most stringent standards.

Adopting Carbon PEEK and ULTEM™ AM9085F enables:

  • Up to 50% weight reduction vs. metals

  • Lower fuel-burn emissions

  • In-house certified production with reduced lead time

Roboze additive manufacturing is redefining lightweight design in aerospace, bringing the precision and reliability of superpolymers to levels once achievable only with metals.

Contact the Roboze Aerospace team today for a free technical-economic evaluation.