DOD SBIR 24.1 BAA

High Temperature Mach number or Static Pressure Probes for Vitiated Flows

ID: AF241-0012Type: BOTH

Overview

Topic

High Temperature Mach number or Static Pressure Probes for Vitiated Flows

Agency

Department of DefenseN/A

Program

Type: SBIRPhase: BOTHYear: 2024

Topic Link

https://www.sbir.gov/node/2479857

Additional Information

https://www.defensesbirsttr.mil/SBIR-STTR/Opportunities/

Timeline

1
Release Nov 29, 2023 12:00 AM
2
Open Jan 3, 2024 12:00 AM
3
Next Submission Due Feb 21, 2024 12:00 AM
4
Close Feb 21, 2024 12:00 AM

Description

The Department of Defense (DOD) is seeking proposals for the topic of "High Temperature Mach number or Static Pressure Probes for Vitiated Flows" as part of their SBIR 24.1 BAA program. The Air Force branch is specifically interested in this topic (AF241-0012). The objective is to develop and demonstrate a local Mach number or Static Pressure probe technology suitable for hypersonic and high enthalpy flows. The technology will be used to understand the test conditions in high-speed hypersonic test facilities and reduce the uncertainty of test results.

In Phase I, the selected proposal will consult with AEDC personnel, survey the industry for potential solutions, and develop the concept and design of the probe technology. Phase II involves developing and demonstrating a prototype probe-rake device in the test facility to demonstrate robustness and accuracy. In Phase III, the technology will be further refined for use within facility rake systems and can be easily commercialized for other high-speed and high-temperature wind tunnels. The project duration is not specified, but the proposal submission deadline is February 21, 2024.

This solicitation presents an opportunity for researchers and companies to contribute to the advancement of hypersonic testing capabilities and potentially commercialize the developed technology. More information can be found on the grants.gov website or the DOD SBIR/STTR Opportunities page.

Files

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