Additively Manufactured Ceramic Rocket Engine Components

Metadata Updated: November 12, 2020

HRL Laboratories, LLC, with Vector Space Systems (VSS) as subcontractor, has a 24-month effort to develop additive manufacturing technology for reinforced ceramic rocket engine components. The technology will be specifically applied to VSS’ LOX/propylene rocket engines in the 800-lbf thrust class and will result in greater than 10 times cost reduction, greater than 10 times reduction in fabrication time and could increase payload by over 10 percent by allowing the integration of complex features that would not be manufacturable otherwise. By maturing this unique process to 3D-print high-temperature ceramics beyond the tipping point for commercialization, a range of aerospace and other applications could benefit from rapid, low-cost fabrication, including upper stage rocket engine chambers/thrusters for small launch vehicles, in-space thrusters for spacecraft, as well as high-temperature components in turbo-pump and combustion devices for larger launch vehicles.We have invented inexpensive pre-ceramic resins that can be printed with conventional stereolithography (SLA) 3D printers [Science Vol 351, p.58 2016]. After printing, the polymer parts can be converted to ceramic by firing in inert atmosphere at 1000-degrees C, offering a 10 times faster and 10 times less expensive method to produce ceramic rocket engine components compared to conventional processing out of ceramic matrix composites. By incorporating fiber reinforcement, the ceramic engine can be toughened and strengthened, averting the brittle fracturing commonly associated with ceramics. Compared to refractory metal-based components, the cost savings are even larger.Our breakthrough in additive manufacturing of polymer-derived ceramics combines the ease, flexibility and low-cost of polymer stereolithography with the high-temperature capabilities of SiC-based ceramics. By avoiding conventional powder-based ceramic processing routes, we will achieve fully dense ceramics with exceptionally high strength. Our most mature 3D-printed silicon oxycarbide (SiOC) ceramic composition exhibits high strength of 300 MPa and survives temperatures of 1700-degrees C for multiple hours. Printed parts can be easily joined in the polymer stage to fabricate ceramic structures that are larger than the build volume of the 3D printer.Together with VSS, HRL will mature the technology from TRL 4 to TRL 6, and scale up fabrication, culminating in hot fire testing of high-performance 800-lbf thrust class LOX/propylene rocket engines with novel designs enabled by additive manufacturing. After successful completion of the program, HRL plans to commercialize the 3D printing technology and make it widely available.

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Metadata Created Date November 12, 2020
Metadata Updated Date November 12, 2020

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Harvested from NASA Data.json

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Resource Type Dataset
Metadata Created Date November 12, 2020
Metadata Updated Date November 12, 2020
Publisher Space Technology Mission Directorate
Unique Identifier Unknown
Maintainer
Identifier TECHPORT_94200
Data First Published 2019-06-01
Data Last Modified 2020-01-29
Public Access Level public
Bureau Code 026:00
Metadata Context https://project-open-data.cio.gov/v1.1/schema/catalog.jsonld
Metadata Catalog ID https://data.nasa.gov/data.json
Schema Version https://project-open-data.cio.gov/v1.1/schema
Catalog Describedby https://project-open-data.cio.gov/v1.1/schema/catalog.json
Homepage URL https://techport.nasa.gov/view/94200
Program Code 026:027
Source Datajson Identifier True
Source Hash 22a338131192cf3f2603543f25f01c2da12f6663
Source Schema Version 1.1

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