# US 10,307,970 B2 · In-situ resource preparation and utilization methods

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- Number: US 10,307,970 B2
- Document ID: US10307970B2
- Status: Granted
- Kind: B2
- Application number: 14/628,040
- Filed: 2015-02-20
- Published: 2015-08-20
- Granted: 2019-06-04
- Earliest claimed: 2014-02-20
- Assignees: Made In Space, Inc.
- Applicants: Made In Space, Inc.
- Inventors: Michael Snyder; Jason Dunn
- Web page: https://patentgrep.com/patent/US10307970B2

## CPC

- B29C 64/165: using a combination of solid and fluid materials, e.g. a powder selectively bound by a liquid binder, catalyst, inhibitor or energy absorber
- B29C 64/321: Feeding
- B33Y 40/00: Auxiliary operations or equipment, e.g. for material handling
- B29L 2009/00: Layered products
- B33Y 10/00: Processes of additive manufacturing
- B33Y 30/00: Apparatus for additive manufacturing; Details thereof or accessories therefor
- B29C: SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING (making preforms B29B11/00; making laminated products by combining previously unconnected layers which become one product whose layers will remain together B32B37/00 - B32B41/00)
- B33Y: ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
- B29L: INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES

## Abstract

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.

## Claims

### Claim 1

A device configured to additively manufacture objects utilizing in-situ materials, the device comprising:
an in-situ material collector configured to collect in-situ material on a celestial body;
a material conditioner, with a receiving area, configured to, at the celestial body, receive collected in-situ material from the in-situ material collector at the receiving area and process 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;
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;
a spooling mechanism configure to spool the filament in-situ material feedstock from the first extruder and to feed the filament in-situ material feedstock; and
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 spooling mechanism, and being configured to, at the celestial body, create at least a portion of an object utilizing the filament in-situ material feedstock.

### Claim 2 (depends on 1)

The device of claim 1, wherein at least a portion of the object is at least a part of a structure or surface.

### Claim 3 (depends on 1)

The device of claim 1, further comprising a descent engine and landing gear allowing landing on the celestial body wherein the celestial body has a microgravity environment.

### Claim 4 (depends on 1)

The device of claim 1, further comprising a binder source supplying at least one of a bioreactor and binder source to the material conditioner.

### Claim 5 (depends on 1)

The device of claim 1, wherein the at least one of the bioreactor and the binder source is an organic binder.

### Claim 6 (depends on 1)

The device of claim 1, wherein the at least a portion of the object includes at least one of: a habitat; a road; a landing pad; a pressure vessel; scaffolding; and an antenna support structure.

### Claim 7 (depends on 1)

The device of claim 1, wherein the first extruder comprises a die.

### Claim 8 (depends on 7)

The device of claim 7, wherein the first extruder comprises heating elements to heat the supply in-situ feedstock being extruded through the die.

### Claim 9

A device configured to additively manufacture a portion of a structure utilizing in-situ materials, the device comprising:
a lander body having landing gear;
an articulating arm, attached to the lander body, having an attached in-situ material collector configured to collect in-situ material on a celestial body;
a material conditioner, attached to the lander body, configured to receive collected in-situ material by placement of the in-situ material at a receiving area by the articulating arm and process the in-situ material;
a first extruder having a first heater, the first extruder configured to receive the processed in-situ material and with a binder form a polymer filament in-situ material feedstock;
a spooling mechanism configured to spool the polymer filament in-situ feedstock material and to feed the polymer filament in-situ material feedstock; and
an additive manufacturing device, attached to the lander body, configured to create the portion of the structure utilizing the filament in-situ material feedstock, the additive manufacturing having a second extruder mounted for positioning on the articulating arm through which the in-situ material feedstock is fed and heated by a second heater to create the portion of the structure layer by layer.

### Claim 10

A device configured to additively manufacture objects utilizing in-situ materials, the device comprising:
an in-situ material collector configured to collect in-situ material on a celestial body with a robotic arm with an end to collect in-situ material from the celestial body having microgravity;
a material conditioner, with a receiving area to accept the collected in-situ material, configured to receive the collected in-situ material from the in-situ material collector and process 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;
a first extruder configured to receive the reduced size in-situ material wherein the reduced size in-situ material with at least one of a bioreactor and a binder source is formed into a supply in-situ material feedstock comprising one of a first filament in-situ material feedstock and a second filament in-situ material feedstock, wherein the second filament in-situ material feedstock includes a metal;
a spooling mechanism configured to spool the supply filament in-situ material feedstock and to feed the one of the supply filament in-situ material feedstock; and
an additive manufacturing device comprising a second extruder and a heating device to at least one of extrude the supply filament in-situ material feedstock feed from the spooling mechanism and to heat the extruded feedstock to create at least a portion of an object layer by layer.

### Claim 11 (depends on 10)

The device of claim 10, wherein at least a portion of the object is at least a part of a surface or infrastructure.

### Claim 12 (depends on 11)

The device of claim 11, further comprising a descent engine and landing gear allowing landing on the celestial body and to which the device is attached during an additively manufacturing process.

### Claim 13 (depends on 11)

The device of claim 11, further comprising a binder source supplying at least one of a bioreactor and binder source.

### Claim 14 (depends on 13)

The device of claim 13, wherein the at least one of the bioreactor and binder source is an organic binder.

### Claim 15 (depends on 11)

The device of claim 11, wherein the device is further configured to additively manufacture infrastructure and the objects include at least one of: a habitat; a road; a landing pad; a pressure vessel; scaffolding; and an antenna support structure.

### Claim 16 (depends on 11)

The device of claim 11, wherein the first extruder comprises a die.

### Claim 17 (depends on 16)

The device of claim 16, wherein the first extruder comprises heating elements to heat the supply in-situ feedstock being extruded through the die.
