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TECHNOLOGY TRANSFER OPPORTUNITY: System for Flight Control of Extremely Fast (Hypersonic) Aircraft (LAR-TOPS-363)

Open — responses due 10 Aug 2027 (287 days left) · Unrestricted (full and open) · National Aeronautics and Space Administration (NASA) · NAICS 927110

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Solicitation details

Notice ID2f72eaa7e1fe41648adb8d01215e740c
AgencyNational Aeronautics and Space Administration (NASA)
Contracting officeNASA MARSHALL SPACE FLIGHT CENTER
NAICS code927110 — Space Research and Technology
Product / service code (PSC)9999
Set-asideUnrestricted (full and open)
Notice typeSpecial Notice
Posted10 August 2026
Response deadline10 August 2027
CompetitionCompetitive

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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: Researchers at NASA s Langley Research Center have designed an electrode-based system for guidance, navigation and control of aircraft or spacecraft moving at hypersonic speeds in ionizing atmospheres. The system is composed of two electrodes that sit on the surface of a craft s thermal protection system (TPS) and an electromagnet positioned beneath the craft s TPS. The system operates based on the principles of magnetohydrodynamics (MHD) and uses energy harvested from the ionized flow occurring during flight at hypersonic speeds to power the electromagnet and generate extremely large Lorentz forces capable of augmenting lift and drag forces to steer and control the craft. The energy harvested can alternatively be stored for later use. NASA s system is simpler than conventional methods for control of hypersonic craft (e.g., chemical propulsion, shifting flight center of gravity, or trim tabs) and enables new entry, descent, and landing mission architectures. NASA s MHD patch technology consists of two electrodes positioned a prescribed distance apart on the surface of the TPS of an aircraft or spacecraft and an electromagnetic coil placed directly below the electrodes with the magnetic field protruding out of the surface. During hypersonic flight, the conductive ionizing atmospheric flow over the surface enables current to flow between the two electrodes. This current is harnessed to power the electromagnet which in turn generates strong Lorentz forces that augment lift and drag forces for guidance, navigation, and control of the craft. Alternatively, the current can be used to charge a battery.? 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/LAR-TOPS-363 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.

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Market context: NASA and NAICS 927110

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Source: this notice on SAM.gov. FedSift republishes public federal procurement data and is not affiliated with the U.S. Government. Always confirm dates and requirements against SAM.gov before responding.