Overkill LEO / GEO / CISLUNAR

Metal, printed for orbit.

We build flight hardware. Generative models design the geometry. Lasers fuse the metal. The parts leave the ground once and never come back.

Capabilities

Structural brackets, propellant manifolds, radiator panels, antenna supports, bus primary structure. Parts that hold spacecraft together and keep them alive through thermal cycling, vacuum, and launch loads.

Each geometry is generated, not drawn. The design space is searched by machine against mass, stiffness, and thermal targets. What survives the search gets printed.

Materials

Ti-6Al-4V

Titanium. Strength to weight. Primary structure and load paths.

IN718

Nickel superalloy. Hot sections, high-stress fittings, fatigue-critical joints.

AlSi10Mg

Aluminum. Thin-wall housings, thermal hardware, mass where it matters least.

CuCrZr

Copper alloy. Conductivity. Heat moves through it or the mission ends.

Process
  1. GenerateConstraints in. Thousands of candidate geometries out. Lattice interiors where solid metal is waste.
  2. PrintLaser powder bed fusion. Layer heights in tens of microns. Melt pool monitored on every pass.
  3. ConsolidateHot isostatic pressing. Porosity closed. Microstructure settled.
  4. FinishInterfaces machined to tolerance. Everything that mates is cut, not printed.
  5. QualifyCT scan of every part. Thermal cycling. Vibration. The part proves itself before it flies.
Position

Mass is the enemy. Every gram is paid for twice — once to make it, once to lift it. We remove everything that does not carry load.

The name is the standard. Margins beyond reason. Parts overbuilt in the only way orbit forgives: lighter, stiffer, and tested past the point anyone asked for.