When is the deadline for the NASA Headquarters RFP?

The deadline for this RFP is Mar 2, 2027. Make sure to submit your proposal before this date to be considered.

What is NASA Headquarters looking for?

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.

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Technology Transfer Licensing Opportunity: Additively Manufactured Propulsion Catalysts (MFS-TOPS-120)

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TECHNOLOGY TRANSFER LICENSING OPPORTUNITY: Additively Manufactured Propulsion Catalysts (MFS-TOPS-120)

Available

NASA Marshall Space Flight Center

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 Date

Mar 24, 2026

Due Date

Mar 2, 2027

View Details →

TECHNOLOGY TRANSFER LICENSING OPPORTUNITY: Additively Manufactured Propulsion Catalysts (MFS-TOPS-120)

Release: Mar 24, 2026

NASA Marshall Space Flight Center

Close: Mar 2, 2027

Available

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Technology Transfer Licensing Opportunity: Conventional Friction Stir Extrusion Machine (MFS-TOPS-126)

Available

NASA Headquarters

Technology transfer licensing opportunity: conventional friction stir extrusion machine.

Posted Date

Mar 24, 2026

Due Date

Mar 2, 2027

View Details →

Technology Transfer Licensing Opportunity: Conventional Friction Stir Extrusion Machine (MFS-TOPS-126)

Release: Mar 24, 2026

NASA Headquarters

Close: Mar 2, 2027

Technology transfer licensing opportunity: conventional friction stir extrusion machine.

Available

View Details →

Technology Transfer Licensing Opportunity: Cladding and Freeform Deposition for Coolant Channel Closeout (MFS-TOPS-81)

Available

NASA Headquarters

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&#8212the 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.

Posted Date

Mar 24, 2026

Due Date

Mar 2, 2027

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Technology Transfer Licensing Opportunity: Cladding and Freeform Deposition for Coolant Channel Closeout (MFS-TOPS-81)

Technology Transfer Licensing Opportunity: 3d-printed Injector for Cryogenic Fluid Management (MFS-TOPS-104)

Available

NASA Headquarters

Developed a system to minimize boil-off during cryogen transfer and storage using an additive manufactured injector with an augmented thermodynamic venting system (TVS). Cryogenic fluid transfer is important for both ground and space-based systems and typically requires venting of a receiver vessel during the chill and fill process to maintain a pressure favorable to fluid flow. NASA's TVS Augmented Injector offers an alternative system that gradually cools the inside of receiving tanks, improving cryogenic fluid transfer and storage efficiency and minimizing or eliminating the time the receiver tank vent needs to be open. The injector is a small piece of 3D-printed hardware that can be easily used with or integrated into tanks or filling equipment in any space or industrial application where a cryogenic fluid is being transferred. The injector may also be employed for long-term cryogenic fluid storage as a means of controlling tank pressure if integrated with a recirculation pump.

Posted Date

Mar 24, 2026

Due Date

Mar 2, 2027

View Details →

Technology Transfer Licensing Opportunity: 3d-printed Injector for Cryogenic Fluid Management (MFS-TOPS-104)

Release: Mar 24, 2026

NASA Headquarters

Summary

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Technology Transfer Licensing Opportunity: Additively Manufactured Propulsion Catalysts (MFS-TOPS-120)

Summary

Key Contacts

What to Include In Your Proposal

Win These Opportunities Next

Files

Contacts & Company Data

Competitor Intelligence

More Opportunities Like This

TECHNOLOGY TRANSFER LICENSING OPPORTUNITY: Additively Manufactured Propulsion Catalysts (MFS-TOPS-120)

TECHNOLOGY TRANSFER LICENSING OPPORTUNITY: Additively Manufactured Propulsion Catalysts (MFS-TOPS-120)

Technology Transfer Licensing Opportunity: Conventional Friction Stir Extrusion Machine (MFS-TOPS-126)

Technology Transfer Licensing Opportunity: Conventional Friction Stir Extrusion Machine (MFS-TOPS-126)

Technology Transfer Licensing Opportunity: Cladding and Freeform Deposition for Coolant Channel Closeout (MFS-TOPS-81)

Technology Transfer Licensing Opportunity: Cladding and Freeform Deposition for Coolant Channel Closeout (MFS-TOPS-81)

Technology Transfer Licensing Opportunity: 3d-printed Injector for Cryogenic Fluid Management (MFS-TOPS-104)

Technology Transfer Licensing Opportunity: 3d-printed Injector for Cryogenic Fluid Management (MFS-TOPS-104)

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