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How Boeing 3D Prints Strong Lightweight Spacecraft Panels

A method for printing a single-piece, high-strength spacecraft panel using 3D printing to create complex internal trusses that eliminate the need for bolts or welds.

Granted 2023ActiveExpires 2039Owned by Boeing CoInvented by Christopher David Joe, Nicole Diane Schoenborn, Richard W. Aston + 1 more

Original patent title: “Additively manufactured spacecraft panel

Plain-English explanation by SahiLast reviewed · June 15, 2026

A method for printing a single-piece, high-strength spacecraft panel using 3D printing to create complex internal trusses that eliminate the need for bolts or welds. Granted to Boeing Co in 2023 with 23 claims.

Key facts

Patent numberUS 11794927
StatusActive
FieldMaterials & Manufacturing
AssigneeBoeing Co
InventorsChristopher David Joe, Nicole Diane Schoenborn, Richard W. Aston and 1 other
Filed2019
Granted2023
Claims23
Times cited0
LitigationNone on record
Value · $26K$84KMinimal

Coverage

What does this patent actually cover?

This patent describes a way to 3D print a spacecraft panel as one single, solid piece. Instead of building a panel from separate sheets and beams, the printer creates two outer skins with stiffening grids and connects them with a complex internal truss structure. Because it is printed as a monolithic unit, the panel has no joints, seams, welds, or fasteners. This design allows for variable density in the internal core, meaning engineers can make parts of the panel stronger or lighter depending on where they are located on the spacecraft.

The gap

What does this patent NOT cover?

  • Does not cover panels built by traditional assembly methods like riveting, welding, or bolting parts together.
  • Does not cover panels that are not produced via additive manufacturing (3D printing).
  • Does not cover structures where the truss members intersect each other, as the claimclaimA numbered sentence at the end of a patent that legally defines what the inventor owns. The most important section.Read more → specifically requires non-intersecting members.
  • Does not cover panels that are not formed as a single monolithic unit.

These exclusions are unique to PatentBrief — derived from the actual claim language, not patent-office boilerplate.

What made this novel

The innovation lies in printing the entire panel—skins and internal truss—as a single monolithic unit where the truss nodes align perfectly with the intersections of the surface stiffeners, all without any internal seams or joints.

Additively manufactured spacec…(Primary claim)aerospacemechanicalmaterials

Schematic visualization of the patent's claim structure. Hand-drawn diagrams in progress for each landmark patent.

Where you've seen this

Real-world examples

01

Satellite chassis structural panels

02

Spacecraft radiation shielding components

03

Lightweight aerospace load-bearing walls

Why it matters

The bigger picture

In space travel, every gram of weight is extremely expensive to launch. By replacing heavy mechanical fasteners and joints with a single, optimized 3D-printed structure, Boeing can reduce the mass of spacecraft components while maintaining structural integrity. This approach represents a shift toward 'part consolidation,' where complex assemblies are reduced to a single printed part, simplifying supply chains and reducing failure points.

Filed

August 28, 2019

Granted

October 24, 2023

Market context

Who's building on this

Companies in this space

Boeing is the primary developer of this technology, using it to refine the structural efficiency of their satellite and spacecraft platforms. Other major aerospace players like Lockheed Martin and various NewSpace startups are also aggressively pursuing additive manufacturing to reduce the weight of orbital hardware.

Market impact

This patent supports the broader industry transition toward additive manufacturing for primary structural components in space. By validating the use of monolithic, joint-free panels, it helps reduce the reliance on complex, labor-intensive assembly processes, potentially lowering the cost of satellite production and increasing the payload capacity of launch vehicles.

Claim 1 — Plain English

What this patent covers

This patent describes a way to 3D print a spacecraft panel as one single, solid piece. Instead of building a panel from separate sheets and beams, the printer creates two outer skins with stiffening grids and connects them with a complex internal truss structure. Because it is printed as a monolithic unit, the panel has no joints, seams, welds, or fasteners. This design allows for variable density in the internal core, meaning engineers can make parts of the panel stronger or lighter depending on where they are located on the spacecraft.

The clever bit

The innovation lies in printing the entire panel—skins and internal truss—as a single monolithic unit where the truss nodes align perfectly with the intersections of the surface stiffeners, all without any internal seams or joints.

What it does not cover

  • Does not cover panels built by traditional assembly methods like riveting, welding, or bolting parts together.
  • Does not cover panels that are not produced via additive manufacturing (3D printing).
  • Does not cover structures where the truss members intersect each other, as the claim specifically requires non-intersecting members.
  • Does not cover panels that are not formed as a single monolithic unit.

Patent timeline

Filing

Application submitted to the patent office

Publication

Application published, typically 18 months after filing

Grant

Patent officially issued

PatentBrief Score

Impact Score

Moderate

Citation count

0/40

No citations yet

Claim breadth

15/20

Broad claimsclaimsThe numbered statements at the end of a patent that legally define what the inventor owns.Read more →

Recency

20/20

Granted within 5 years

Assignee scale

20/20

Major company or institution

PatentBrief Impact Score — based on citation count, claim breadth, recency, and assignee scale. Not a legal assessment.

Heuristic Value Estimate

What this patent might be worth

Minimal

$26K$84K

Midpoint $53K · 13.2 yr remaining · industry ×0.9

Adjust inputs →

Heuristic only — blends forward/backward citation counts, claim scope, time remaining, litigation history, and CPC-derived industry baseline. Real valuations need a professional appraisal.

The original legal language

Original claims

23 claims as filed with the patent office.

Concepts involved

ClaimPrior artNon-obviousnessNoveltySpecificationAssigneePatent term

Citations

Patent lineage

Cites earlier patents

81

earlier patents this invention cites as foundations

View prior art →

Cite this patent

Joe, C. D., Schoenborn, N. D., Aston, R. W., & Hastings, N. M. (2023). How Boeing 3D Prints Strong Lightweight Spacecraft Panels (U.S. Patent No. 11,794,927). U.S. Patent and Trademark Office. https://patentbrief.org/patent/us/11794927/starship-life-support-system

Auto-generated from the patent record. Double-check author order and the issue date against the official USPTO document before submitting.

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Common Questions

Frequently Asked Questions

What does How Boeing 3D Prints Strong Lightweight Spacecraft Panels cover?

A method for printing a single-piece, high-strength spacecraft panel using 3D printing to create complex internal trusses that eliminate the need for bolts or welds.

Who owns patent US 11794927?

Boeing Co owns this patent, granted in 2023.

When does this patent expire?

This patent is expected to expire on October 24, 2043, when the invention enters the public domain.

What problem does this patent solve?

In space travel, every gram of weight is extremely expensive to launch. By replacing heavy mechanical fasteners and joints with a single, optimized 3D-printed structure, Boeing can reduce the mass of spacecraft components while maintaining structural integrity. This approach represents a shift toward 'part consolidation,' where complex assemblies are reduced to a single printed part, simplifying supply chains and reducing failure points.

What does this patent NOT cover?

Does not cover panels built by traditional assembly methods like riveting, welding, or bolting parts together.

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Last reviewed: June 15, 2026 · PatentBrief is not a law firm and this is not legal advice.