Physics, Materials & Applied Math Resear

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SBIR Award Summary

Total Number of Awards 41
Total Value of Awards $12.2MM
First Award Date 01/01/00
Most Recent Award Date 02/03/16

Key Personnel

Last Name Name Awards Contact
Reed Helen Reed 2 Message
Kremeyer Dr. Kevin Kremeyer 33 Message
Tichenor Nathan Tichenor 8 Message
Chiang Margaret Chiang 9 Message
Mickelson Pascal Mickelson 1 Message
Yeak Jeremy Yeak 1 Message

41 Awards Won

Phase 1 SBIR

Agency: Department of Defense
Topic: DTRA143-009
Budget: 02/03/16 - 09/03/16

We propose the development new kind of high resolution tunable spatial heterodyne spectrometer for nuclear forensics. Preliminary results have shown that this spatial heterodyne spectrometer can be made compact without sacrificing its high resolving power for isotopic attribution of nuclear materials. Thus, the spatial heterodyne spectrometer wi...

Phase 1 SBIR

Agency: Army
Topic: A15-079
Budget: 09/16/15 - 03/15/16

The proposed effort is geared toward developing an ultrashort pulse beam director for ground to ground and ground to air engagements, with a particular focus on material identification and remote sensing.

Phase 1 STTR

Institution: Texas A&M University

Agency: Air Force
Topic: AF15-AT39
Budget: 08/04/15 - 05/09/16

ABSTRACT: The ability to convert extreme aerodynamic heating into electricity via thermoelectric generators presents a unique opportunity to leverage this otherwise undesirable condition. The harvested energy can be used to power the significant electrical demand of a hypersonic/long range vehicle while also aiding in managing high temperatures....

Phase 1 SBIR

Agency: Department of Energy
Topic: 32e
Budget: 06/08/15 - 03/07/16

Long-term corrosion of steel in concrete structures is a particular concern for nuclear power plants as there is a compelling public interest in the safe operation of these plants for the many decades that they are in operation and the additional decades it takes for them to be decommissioned. Inspection techniques that are both non-destructive ...

Phase 1 STTR

Institution: University of Houston

Agency: Air Force
Topic: AF15-AT31
Budget: 01/01/15 - 12/31/15

ABSTRACT: This proposal translates a non-toxic, aqueous-based, near room temperature electrodeposition process to completely eliminate Cr (VI) for the production of wear and corrosion resistant surfaces on high-strength steel. Specifically, our process will produce adherent and crack-free Re-based coatings that are extremely high-temperature (Tm...

Phase 1 STTR

Institution: Texas A&M University

Agency: Navy
Topic: N14A-T004
Budget: 09/09/14 - 04/09/15

Combustion instability, or screech, occurs in many modern gas turbine systems, and is due to the complex physical coupling of the acoustic resonances in the combustion chamber with fluctuations in the heat release of the combustion process. These instabilities can produce large pressure fluctuations that can be severe enough to damage engine har...

Phase 1 SBIR

Agency: Air Force
Topic: AF131-192
Budget: 02/03/14 - 11/02/14

The proposed effort will investigate and develop a laser-scopic tool that will provide earlier and improved capabilities for corrosion-detection, -removal, -cleaning and -repair due to galvanic couples in hard-to-access areas, without damaging the underlying substrate or adjacent features. The key focus areas include system definition, power-de...

Phase 1 STTR

Institution: Texas A&M University

Agency: Navy
Topic: N14A-T004
Budget: 01/01/14 - 12/31/14

Combustion instability, or screech, occurs in many modern gas turbine systems, and is due to the complex physical coupling of the acoustic resonances in the combustion chamber with fluctuations in the heat release of the combustion process. These instabilities can produce large pressure fluctuations that can be severe enough to damage engine har...

Phase 2 SBIR

Agency: Air Force
Topic: AF121-191
Budget: 01/01/14 - 12/31/14

ABSTRACT: Hypersonic propulsion systems, such as supersonic combustion ramjets (scramjets) are generally expected to operate from Mach 3.5 up to Mach 7-8 and are designed for specific flight Mach numbers to achieve optimum performance. However, realistic flight vehicles will experience a wide range of flight conditions during a typical mission....

Phase 2 SBIR

Agency: Air Force
Topic: AF121-191
Budget: 11/07/13 - 02/04/16

ABSTRACT: Hypersonic propulsion systems, such as supersonic combustion ramjets (scramjets) are generally expected to operate from Mach 3.5 up to Mach 7-8 and are designed for specific flight Mach numbers to achieve optimum performance. However, realistic flight vehicles will experience a wide range of flight conditions during a typical mission. ...

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