TECHNOLOGY TRANSFER OPPORTUNITY: Aerospace Vehicle Entry Flightpath Control (TOP2-303)
Special Notice from National Aeronautics and Space Administration.
Data as of Oct 24, 2026. Sources: SAM.gov and Grants.gov. Snapshot govcon-directory-20261024T104923Z-2151694.
This product uses the Grants.gov API but is not endorsed or certified by the U.S. Department of Health and Human Services. Counts and totals are computed by DSE from public SAM.gov and Grants.gov notices. Text from Grants.gov may be shortened or have contact details removed. The original notice on Grants.gov is the authoritative version.
Closing in 290 days
Notice details
- Sub-tier agency
- NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
- Notice type
- Special Notice
- Solicitation number
- T2P-ARC-00124
- Product/service code
- 9999
- Posted
- Aug 11, 2026
- Response deadline
- Aug 10, 2027
- Source
- SAM.gov
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: The state-of-the-art in hypersonic entry Guidance and Control (G&C) is traditionally based on rigid entry vehicles, like the Orion capsule, Space Shuttle, etc., that use a Reaction Control System (RCS) to control the bank angle of the vehicle. However, for future high mass missions to Mars, advancements in hypersonic aerospace vehicle design, and evolving science goals, are stretching the performance capabilities of traditional entry systems. NASA�s Pterodactyl team at Ames Research Center has developed a novel yaw-to-bank control system for a non-traditional vehicle configurations, such as a Deployable Entry Vehicle (DEV) that can be folded and stowed. The approach provides vehicle stabilization, steering, and precise targeted landing. This control architecture is agnostic to control actuators and can be used with any aerospace vehicle with a strong dihedral effect and/or different guidance control variables. This novel flightpath control system exploits the dihedral effect to control the bank angle of the vehicle by modulating sideslip. Exploiting the dihedral effect, in combination with significant aerodynamic
Summarized from the official notice. The description is shortened; read the full text on the official notice.
Official notice
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When is the response deadline?
The published deadline is Aug 10, 2027. That is 290 days after the data date.
What NAICS code applies?
NAICS 927110, Space Research and Technology.
Which agency issued this notice?
National Aeronautics and Space Administration.
Where is the official notice?
The link under Official notice opens the source listing.