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Space

Rockets and spacecrafts endure extreme heat, erosion, and micro-debris impacts, resulting in costly refurbishments per launch.

 

Our novel materials extend the lifecycle of critical components by resisting thermal shock, oxidation, and certain orbital impacts - enhancing spacecraft survivability,  lowering costs per launch, and driving rapid reusability.

Visual shown is a conceptual application demonstration

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  • Safeguards propellant tanks, feedlines, and valves from cryogenic cycling, liquid fuel exposure, and hydrogen-induced cracking.

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Ablation
& Surface Erosion

  • Extends life of rocket fairings, and structual joints by resisting ablation, plasma erosion, and gas shear effects.

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Micrometeoroid & Debris Impact

  • Shields satellite structures and spacecraft hulls from high-velocity particle strikes and small orbital debris penetration.

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Thermal Fatigue & Oxidation

  • Protects cryogenic tanks, valves, and feedlines from repeated chill–heat cycles and oxidative stress during launch and re-entry.

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Space Applications

Propulsion & Power Systems

  • Engine Throat Wear Layers (outer protective coat only)

  • Turbopump Bearings, Shafts & Housings

  • Fuel Injectors & Injector Plates

  • Cryogenic Pump Impellers & Valve Components

  • Power Generation Turbines

  • Electric Propulsion Thruster Components 

Thermal Protection & Structures

  • Fuselage / Outer Hull Micrometeoroid Shielding

  • Structural Joints & Fasteners (thermal cycling & oxidation control)

  • Internal Tank Surfaces (thermal fatigue resistance)

  • Secondary Frames & Load-Bearing Members (oxidation/erosion resistance)

Orbital & Control Systems

  • Satellite Thruster Components (cold-gas, monoprop, biprop)

  • Reaction Wheel Bearings & Housings

  • Solar Array Hinges & Deployment Mechanisms

  • Attitude Control System Valves & Actuators

  • Antenna / Sensor Gimbal Bearings

Fuel & Fluid Systems

  • Cryogenic Tank Linings (LOX, LH₂, CH₄)

  • High-Pressure Lines & Fittings

  • Pump & Valve Internals (propellant feed systems)

  • Manifolds & Distribution Blocks

  • Heat Exchanger Surfaces (fuel preburner loops)

Environmental & Survivability

  • Micrometeoroid & Orbital Debris Shields (sacrificial outer layers)

  • Anti-oxidation Coatings for Long-Duration Orbits (LEO/GEO)

  • Radiation-Resistant Coatings for Electronics Housings

  • Thermal Radiator Panels (oxidation & atomic oxygen resistance)

  • Protective Coatings for Docking Mechanisms

Get Involved

Engage with Mjolner today by requesting a sample.

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Spacecraft : Micrometeoroid impact (2-3mm 7km/s), Immunity to Particle impact

Landing Gear & Structural Joints (Reusable Boosters) : Fatigue resistance +40%, Refurbishment time reduction +25%

Reaction Wheels & Bearings : Component life +40%, Reduced in-orbit failures +30%

Fuel Pump & Valve Internals (Cryogenic) : Reliability +40%, Overhaul cycle extension +30%

Re-entry Heat Shields (non-thrust surfaces) : Thermal shock resistance +25%, Crack/erosion prevention +20%

Payload Bay & Fairing Liners : Erosion resistance +30%, Cleaning/turnaround time reduction +25%

 

"Performance data represents estimated ROIs based on publicly available sources and benchmark studies. Actual results will vary on a case-by-case basis."

Application Methods - The Process

Our Tailored Coating Process

  1. You Define the Mission: Tell us your component and performance requirements.

  2. We Engineer & Sample: We customize material formulations & methods and deliver test samples.

  3. You Validate: Run your application-specific tests; if needed, we refine the formulation.

  4. We Finalize & Deliver: Lock in coating methods, process your parts, and share the performance data.

 

We are here to Precisely Tuned to Your Needs.

Thermal Spray

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Cold Spray

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PVD

HVOF/HVAF

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Laser Cladding

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