# TECHNOLOGY TRANSFER OPPORTUNITY: Supersonic Spike Diffuser (SSC-TOPS-10)

Notice 7601cb72ff5144858f6a024dbfc4fcec (solicitation TP2-SSC-00009) from NATIONAL AERONAUTICS AND SPACE ADMINISTRATION, NASA MARSHALL SPACE FLIGHT CENTER, posted 2026-08-10, responses due 2027-08-10T20:00:00.000Z. Status: open.

| Field | Value |
| --- | --- |
| Notice ID | 7601cb72ff5144858f6a024dbfc4fcec |
| Solicitation number | TP2-SSC-00009 |
| Type | Special Notice |
| Agency | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION |
| Sub-tier | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION |
| Office | NASA MARSHALL SPACE FLIGHT CENTER |
| Posted | 2026-08-10T22:32:15.000Z |
| Response deadline (UTC) | 2027-08-10T20:00:00.000Z |
| Set-aside | - |
| NAICS | 927110 |
| PSC | 9999 |
| Place of performance | - |
| Award | - |

## 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: Standard cylindrical and second-throat diffusers allow supersonic gas flows to expand within their walls and pull a vacuum on any upstream void. However, the high-Mach-number shock reflections that occur in the center of the plume create substantial losses and result in an inefficient pumping process. Centerbody diffuser designs provide an improvement by reducing the maximum Mach number of the core flow, but also increase the number of oblique shocks in the system by introducing multiple turns into the system. A new type of spike diffuser recently developed by NASA Stennis Space Center is able to provide approximately double the pumping performance of second-throat diffusers via Pareto-efficient reduction of both core Mach number and flow deflection. This enables substantially lower vacuum pressures to be achieved for a given feed pressure/mass flow via the use of higher-expansion-ratio driving nozzles. Spike diffusers are also spatially compact, requiring only ~25% of the length of second-throat designs. To express interest in this opportunity, please submit a license application through NASA’s Automated Technology Licensing Application System (ATLAS) by visiting https://technology.nasa.gov/patent/SSC-TOPS-10 If you have any questions, please e-mail NASA’s Technology Transfer Program at Agency-Patent-Licensing@mail.nasa.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.

## Sources

- View on SAM.gov: https://sam.gov/opp/7601cb72ff5144858f6a024dbfc4fcec/view
- Data as of 2026-11-14. Source: https://sam.gov/data-services/Contract%20Opportunities/datagov

## Cite this

"TECHNOLOGY TRANSFER OPPORTUNITY: Supersonic Spike Diffuser (SSC-TOPS-10), SAM.gov contract opportunity 7601cb72ff5144858f6a024dbfc4fcec." samgovapi.io, https://samgovapi.io/opportunity/7601cb72ff5144858f6a024dbfc4fcec, data as of 2026-11-14. Primary record: https://sam.gov/opp/7601cb72ff5144858f6a024dbfc4fcec/view

## API and MCP

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