TECHNOLOGY TRANSFER LICENSING OPPORTUNITY: A One-piece Liquid Rocket Thrust Chamber Assembly (MFS-TOPS-93)
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NASA is seeking interested companies to obtain licensing rights for a one-piece regeneratively-cooled thrust chamber assembly designed for liquid rocket engines. Developed under the Rapid Analysis and Manufacturing Propulsion Technology project, this innovation utilizes 3D printing and large-scale additive manufacturing to eliminate complex joints, reducing the risk of catastrophic seal failures and decreasing overall weight by over 40 percent through the use of a composite overwrap. License rights may be granted on an exclusive or nonexclusive basis, though NASA provides no funding in conjunction with these licenses. Interested parties must submit applications through the Automated Technology Licensing Application System by March 2, 2027. This opportunity is intended to foster public-private partnerships that strengthen the US supply chain for reliable spaceflight hardware.
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Full Description
NASA’s Technology Transfer Program solicits inquiries from companies interested in obtaining license rights to commercialize, manufacture and market the following technology. License rights may be issued on an exclusive or nonexclusive basis and may include specific fields of use. NASA provides no funding in conjunction with these potential licenses.
THE TECHNOLOGY:
NASA is developing a lightweight one-piece regeneratively-cooled thrust chamber assembly (TCA) for liquid rocket engines. Liquid rocket engines create thrust through the expansion of combusted propellants within the TCA. Standard manufacturing of TCAs involves individually building the injector, main combustion chamber and nozzle, and then bolting or welding the components together at the joints. However, potential seal failures in these complex joints can cause catastrophic explosions, as in the tragedy of the Space Shuttle Challenger. NASA researchers are eliminating complex joints by manufacturing a 1-piece TCA utilizing 3D printing and large-scale additive manufacturing technologies to directly deposit the nozzle onto the combustion chamber. And, by replacing a traditional solid metal jacket with a composite overwrap for support, the overall weight is reduced by over 40%. Developed under the Rapid Analysis and Manufacturing Propulsion Technology (RAMPT) project, NASA seeks public-private partnerships to develop specialized large-scale additive manufacturing vendors and accelerate reliable spaceflight hardware to the US supply chain.
To express interest in this licensing opportunity, please submit a license application through NASA’s Automated Technology Licensing Application System (ATLAS) by visiting https://technology.nasa.gov/patent/MFS-TOPS-93
If you have any questions, please e-mail NASA’s Technology Transfer Program at contact@example.gov with the title of this Technology Transfer Opportunity as listed in this SAM.gov notice and your preferred contact information. For more information about licensing other NASA-developed technologies, please visit the NASA Technology Transfer Portal at https://technology.nasa.gov/
These responses are provided to members of NASA’s Technology Transfer Program for the purpose of promoting public awareness of NASA-developed technology products, and conducting preliminary market research to determine public interest in and potential for future licensing opportunities. No follow-on procurement is expected to result from responses to this Notice.
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