Rocket Hangar
System Status: Nominal

BUILDING
MACH 5

Engineering the next generation of orbital propulsion componentsfor mission-critical payloads.

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MISSION HARDWARE

// CATALOG_ID: 2024-ALPHA
Select components for detailed telemetry and specifications.

Vulkan-X Nozzle
Propulsion

Vulkan-X Nozzle

Additively manufactured Inconel 718 with regenerative cooling channels.

Cryo-Pump Mk. IV
Fuel Delivery

Cryo-Pump Mk. IV

High-pressure turbopump for LOX/Methane cycles.

Metallurgy

Material Spec: Inconel 718

Heat treated for max tensile strength at 900°C.

Performance

5,000°K

Thermal Resistance

Carbon Composite Airframe
Structure

Carbon Composite Airframe

Filament-wound pressure vessels for orbital stage.

Engineering Breakdown

VULKAN-X ASSEMBLY

Injector Plate

Cryogenic flow stabilization pattern.

Combustion Chamber

Regeneratively cooled Inconel alloy.

Exit Nozzle

Vacuum optimized expansion ratio.

R&D Protocols

Manufacturing Matrix

Electroforming
Dataset: Electroforming

Electroforming

Atomic-level precision for complex geometries. Our electroforming process delivers seamless components with extreme tolerance control.

  • Atomic Precision
  • Complex Geometries
  • Seamless Structure
Deep Draw
Dataset: Deep Draw

Deep Draw

Seamless metal forming for high-pressure tanks. We specialize in deep draw fabrication for cryogenic and propellant storage.

  • High Pressure
  • Uniform Thickness
  • Scalable Production
Spin Forming
Dataset: Spin Forming

Spin Forming

Symmetric perfection for nose cones and fairings. Advanced spin forming for aerodynamic excellence.

  • Symmetric Perfection
  • Large Diameter
  • High Strength