Back to results
US 2026/0063334 A1Published application
Systems and methods for manufacturing in space environments
AssigneeTrans Astronautica Corporation
InventorsJoel C. Sercel, Philip J. Wahl, James G. Small
Life of this patent
Estimating the term…
Abstract
A factory for manufacturing useful products while orbiting is space uses concentrated solar energy, high vacuum, and the low temperatures available in a space environment. Gyroscopic forces from rotating machinery are carefully controlled. Liquids, gases, and solid minerals are separated from asteroid and lunar regolith resources.
Claims18
(canceled)
A system for fabricating fibers in space, comprising:
- a containment vessel configured to contain feedstock materials obtained from an asteroid or lunar regolith;
- one or more optical components configured to collect solar energy from the Sun, concentrate the collected solar energy, and direct the concentrated solar energy to impinge upon a surface of the feedstock materials to melt the feedstock materials;
- and
- a piston configured to apply a pressure to the melted feedstock materials to extrude the melted feedstock materials through an orifice in the containment vessel to produce an extrusion.
1 more element
A system for separating materials in space, comprising:
- a smelting vessel configured to contain feedstock materials obtained from an asteroid or lunar regolith, the feedstock materials including a first material and a second material;
- one or more optical components configured to collect solar energy from the Sun, concentrate the collected solar energy, and direct the concentrated solar energy to impinge upon a surface of the feedstock materials to melt the feedstock materials;
- and
- a motor configured to spin the smelting vessel to separate the melted feedstock materials into the first material and the second material.
1 more element
A vapor phase deposition (VPD) orbiting factory in space, comprising:
- a crucible configured to hold an ingot of feedstock, the crucible comprising pores;
- a form in the shape of a structure to be fabricated;
- and
- a solar concentrator configured to concentrate solar power to a concentration ratio sufficient to vaporize the feedstock within the crucible, the vaporized feedstock passing through the pores in the crucible and depositing onto the form.
1 more element
A method of forming a structure, comprising:
- receiving an asteroid at an orbiting factory in space;
- vaporizing the asteroid using concentrated solar energy to produce a feedstock material;
- loading the feedstock material into a vapor phase deposition (VPD) crucible;
- vaporizing the feedstock material within the VPD crucible with concentrated solar power;
- and
- forming the structure with the vaporized feedstock material.
3 more elements
Dependencies are inferred from the claim text.