Description
The National Aeronautics and Space Administration (NASA) is seeking a custom 3-channel constant-temperature-anemometer (CTA) system for supersonic and hypersonic flow measurements. The system should provide high-bandwidth flow measurements with low system noise, outperforming commercially available systems in the US. The project involves developing a 3-channel CTA system based on an earlier functional system, with minor adjustments to improve user experience. The primary deliverable is a second three-channel CTA system, along with a user manual. The work schedule is expected to be approximately 5 months from contract award.
Key aspects of the project include:
• Developing a custom 3-channel CTA system
• Providing high-bandwidth flow measurements in supersonic and hypersonic flow regimes
• Maintaining low system noise
• Delivering a user manual and a second three-channel CTA system
• Completing the project within approximately 5 months from contract award
Attached files
Contact
Shanna Patterson