In-situ resource preparation and utilization methods
Methods of collecting in-situ materials on a celestial body for return to Earth or another location and associated devices are described. These devices and methods facilitate collection of samples and creation of portions of the return spacecraft via an additive manufacturing device contained within the lander craft. The additive manufacturing device is configured to produce portions of the return spacecraft (e.g., sample return container, spacecraft structure, heat shield) and may also be configured to place samples within the spacecraft for return and analysis.
1. A method of utilizing in-situ materials on a celestial body as a portion of an object, the method comprising:
collecting in-situ material on the celestial body with an in-situ material collector;
processing, on the celestial body, the collected in-situ material with a material conditioner with a receiving area to receive collected in-situ material from the in-situ material collector by at least reducing the in-situ material to a dimension smaller than the in-situ material as collected with at least one of a grinder, a shifter and a chemical to produce a reduced size of the in-situ material;
conditioning, on the celestial body, the reduced in-situ material with a first extruder configured to receive the reduced size in-situ material wherein the reduced size in-situ material is combined with at least one of a bioreactor and a binder source to form a filament in-situ material feedstock;
dispensing the filament in-situ material feedstock with a mechanism configured to provide from the first extruder the filament in-situ material feedstock; and
creating at least a portion of the object utilizing the filament in-situ material feedstock with an additive manufacturing device comprising at least a second extruder to extrude the filament in-situ material feedstock feed to the second extruder from the mechanism.
2. The method according to claim 1 , wherein the at least one of the bioreactor and the binder source comprises an organic binder.
3. The method according to claim 1 , wherein the object comprises a spacecraft.
4. The method according to claim 3 , further comprising:
collecting a material sample from the celestial body with a robotic arm; and
placing the collected material sample within the spacecraft.
5. The method according to claim 4 , further comprising placing the collected material sample within a sample container within the spacecraft wherein the sample container is created with claim 1 .
6. The method according to claim 3 , further comprising launching the spacecraft on a return trajectory to Earth.
7. A method of utilizing in-situ materials on a celestial body as a portion of an object, the method comprising:
collecting in-situ material on a celestial body with a robotic arm having at least one end to collect in-situ material from the celestial body having microgravity;
accepting the collected in-situ material at a material conditioner having a receiving area;
processing the in-situ material by at least reducing the in-situ material to a dimension smaller than the in-situ material as collected with at least one of a grinder, a shifter and a chemical to produce a reduced size of the in-situ material;
creating a supply in-situ material feedstock with a first extruder by combining at least one of a bioreactor and a binder source with the reduced size in-situ material wherein the supply in-situ material feedstock comprises at least one of a first filament in-situ material feedstock and a second filament in-situ material feedstock;
at least one of storing and releasing at least one of the first filament in-situ material feedstock and the second filament in-situ material feedstock with a mechanism; and
creating at least a portion of the object with an additive manufacturing device comprising a second extruder to extrude the supply filament in-situ material feedstock and a heating device to heat the extruded feedstock to provide for creation.
8. The method according to claim 7 , further comprising supplying a metallic material to provide for at least one of the first filament in-situ material feedstock and the second filament in-situ material feedstock comprising the metallic material.
9. The method according to claim 7 , wherein the at least one of the bioreactor and binder source is an organic binder.
10. The method according to claim 7 , wherein the object comprises a spacecraft.
11. The method according to claim 10 , further comprising:
collecting a material sample from the celestial body with a robotic arm; and
placing the collected material sample within the spacecraft.
12. The method according to claim 11 , further comprising placing the collected material sample within a sample container within the spacecraft wherein the sample container is created with claim 1 .
13. The method according to claim 11 , further comprising launching the spacecraft on a return trajectory to Earth.
14. A method of utilizing in-situ materials on a celestial body as a portion of an object, the method comprising:
collecting in-situ material on the celestial body with an in-situ material collector;
processing, on the celestial body, the collected in-situ material with a material conditioner with a receiving area to receive collected in-situ material from the in-situ material collector by at least reducing the in-situ material to a dimension smaller than the in-situ material as collected with at least one of a grinder, a shifter and a chemical to produce a reduced size of the in-situ material;
conditioning, on the celestial body, the reduced in-situ material with a first extruder configured to receive the reduced size in-situ material wherein the reduced size in-situ material is combined with at least one of a bioreactor and a binder source to form a filament in-situ material feedstock;
dispensing the filament in-situ material feedstock with a mechanism configured to provide from the first extruder the filament in-situ material feedstock; and
creating at least a portion of the object utilizing the filament in-situ material feedstock with an additive manufacturing device comprising at least a second extruder to extrude the filament in-situ material feedstock feed to the second extruder from the mechanism wherein the object comprises a spacecraft.
15. The method according to claim 14 , wherein the at least one of the bioreactor and the binder source comprises an organic binder.
16. The method according to claim 14 , further comprising:
collecting a material sample from the celestial body with a robotic arm; and
placing the collected material sample within the spacecraft.
17. The method according to claim 16 , further comprising placing the collected material sample within a sample container within the spacecraft wherein the sample container is created with claim 14 .
18. The method according to claim 14 , further comprising launching the spacecraft on a return trajectory to Earth.