Posted
Mar 24, 2026
Mar 2, 2027
Technology Transfer Licensing Opportunity: Conventional Friction Stir Extrusion Machine (MFS-TOPS-126)
Technology transfer licensing opportunity: conventional friction stir extrusion machine.
Description: NASA Marshall Space Flight Center issued a Technology Transfer licensing notice for a Conventional friction stir extrusion machine (MFS-TOPS-126), offering license rights to commercialize and manufacture the technology. The notice explicitly states that NASA provides no funding in conjunction with potential licenses and requires interested parties to submit applications via the ATLAS portal. The opportunity was published on March 24, 2026, with a final response deadline of March 2, 2027.
Federal · DC, US
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Posted
Mar 24, 2026
Mar 2, 2027
Technology transfer licensing opportunity: conventional friction stir extrusion machine.
Posted
Mar 24, 2026
Mar 2, 2027
In mono-propulsion systems, a propellant is flowed across a catalyst to promote a chemical reaction and generate thrust. Conventional catalyst manufacturing methods entail (a) coating the inner walls of the thruster nozzle with a catalyst (generally undesirable due to limited catalyst-propellant contact), or (b) inserting a metal or graphite foam coated with a catalyst material into the thruster chamber. Method (b), while superior in terms of thrust generation, also possesses several limitations. Metal/graphite foams are difficult and expensive to procure, stochastic/random in nature (e.g., possess high variability in terms of geometric and other properties), and must be jammed into the thruster chamber using a compression plunger during installation – a process that often leads to catalyst damage. A new manufacturing method that improves repeatability, thruster reactivity, and tailorability (e.g., mechanical, chemical, and fluid flow) while reducing cost and lead time is thus highly desirable. To address this need, NASA and EOS developed methods to additively manufacture (AM) ultra-fine lattice structure propulsion catalysts.
NASA Marshall Space Flight Center
FederalAL
Posted
Mar 24, 2026
Mar 2, 2027
NASA Marshall Space Flight Center (MSFC) is soliciting expressions of interest for licensing rights to commercialize additively manufactured propulsion catalyst technology (MFS-TOPS-120). NASA provides no funding and requests license applications via its ATLAS system (https://technology.nasa.gov/patent/MFS-TOPS-120). Responses are due March 2, 2027 at 4:00 p.m. EST and the notice is currently open.
Posted
Mar 24, 2026
Mar 2, 2027
Low-cost, large-scale liquid rocket engines with regeneratively cooled nozzles will enable reliable and reduced-cost access to space. Coolant, contained under high pressure, circulates through a bank of channels within the nozzle to properly cool the nozzle walls to withstand high temperatures and prevent failure. It has been a challenge to affordably manufacture and close out the intricate nozzle channels. As such, NASA developed a robust and simplified additive manufacturing technology to build the nozzle liner outer jacket to close out the channels within and contain the high-pressure coolant. The new Laser Wire Direct Closeout (LWDC) capability reduces the time to fabricate the nozzle and allows for real-time inspection during the build. One variation enables a bimetallic part (copper/super-alloy, e.g.) to help optimize material where it is needed. The manufacturing process has been demonstrated on a series of different alloys. Hot-fire testing is complete—the parts were exposed to extreme combustion chamber temperatures and pressure conditions for 1,000+ seconds. Micro-graph examination of the hot-fired test article has verified that the coolant channel closeout bonds are reliable and that there is very little deformation to the coolant channels.