Tetra Research Corporation
CAGE Code: 088X4
NCAGE Code: 088X4
Status: Active
Type: Commercial Supplier
Dun & Bradstreet (DUNS): 969308311
Summary
Tetra Research Corporation is an Active Commercial Supplier with the Cage Code 088X4 and is tracked by Dun & Bradstreet under DUNS Number 969308311..
Address
4013 Lakepoint Rd
Champaign IL 61822-9761
United States
Points of Contact
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Frequently Asked Questions (FAQ) for CAGE 088X4
- What is CAGE Code 088X4?
- 088X4 is the unique identifier used by NATO Organizations to reference the physical entity known as Tetra Research Corporation located at 4013 Lakepoint Rd, Champaign IL 61822-9761, United States.
- Who is CAGE Code 088X4?
- 088X4 refers to Tetra Research Corporation located at 4013 Lakepoint Rd, Champaign IL 61822-9761, United States.
- Where is CAGE Code 088X4 Located?
- CAGE Code 088X4 is located in Champaign, IL, USA.
Contracting History for CAGE 088X4 Most Recent 25 Records
- 80NSSC21C0577
- Advanced Computational Tools For Thermal And Acoustic Analysis Of Rocket Ground Test Facilities
- 28 Jul 2021
- Advanced Computational Tools For Thermal And Acoustic Analysis Of Rocket Ground Test Facilities
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,997.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0577
- Eo14042 Advanced Computational Tools For Thermal And Acoustic Analysis Of Rocket Ground Test Facilities.
- 15 Oct 2021
- Eo14042 Advanced Computational Tools For Thermal And Acoustic Analysis Of Rocket Ground Test Facilities.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,997.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC20C0245
- Algorithmic Improvements For Cryogenic Fluid.Management Applications
- 10 Feb 2022
- Algorithmic Improvements For Cryogenic Fluid.Management Applications
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $250,000.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC20C0245
- Algorithmic Improvements For Cryogenic Fluid.Management Applications
- 20 Aug 2020
- Algorithmic Improvements For Cryogenic Fluid.Management Applications
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $250,000.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC20C0523
- Advanced Computational Tools For Thermal And Acoustic Analysis Of Rocket Ground Test Facilities
- 12 Aug 2020
- Advanced Computational Tools For Thermal And Acoustic Analysis Of Rocket Ground Test Facilities
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,999.00
- National Aeronautics And Space Administration (Nasa)
- NNX17CS03C
- Rigorous Ground Testing Mitigates Space Propulsion System Risk By Enabling Advanced Component And System Level Rocket Propulsion Development And By Demonstrating That Designs Reliably Meet The Specified Requirements Over The Operational Envelope Before The First Flight. The Development Of Advanced Ground Test Technology Components And Systems That Are Capable Of Enhancing Environment Simulation, Minimizing Program Test Time, Cost And Risk And Meeting Environmental And Safety Regulations Is Focused On Near-Term Products That Augment Existing State-Of-The-Art Propulsion System Test Facilities. Thus Improved Capabilities To Model And Predict Component Behavior In Harsh Ground Test Environments Are Needed For Enhanced Facility Design. In Particular, Components Such As Pumps, Turbines, Valves And Chokes May Experience Vibration And Damage Due To Cavitation In The Flowing Liquid, And Any Reduction In The Severity Of The Operating Conditions Would Provide Expanded Test And Performance Benefits. The Proposed Innovation Is To Develop An Unsteady Cavitation Model Based On A Tabular Equation Of State And A Representation Of Cavitation Bubble Dynamics That Together Describe The Growth And Collapse Of Nucleated Bubbles In A Liquid Cryogen. Important Nonequilibrium Mechanical And Thermal Effects Will Be Considered By Using A Drift-Flux Model And Adding An Additional Energy Equation For The Liquid Temperature. Validation Of The Advanced Cavitation Models Will Be Accomplished For Both Steady And Unsteady Flows By Comparing Surface Pressure And Temperature Data And Computing Power Spectra From Frequency Domain Analyses. The Final Analysis Tool Will Be Used To Demonstrate The Significant Nonequilibrium Flow Behavior For Both The Validation Cases And Actual Production Analysis Problems Of Interest To Nasa.
- 4 Jun 2018
- Rigorous Ground Testing Mitigates Space Propulsion System Risk By Enabling Advanced Component And System Level Rocket Propulsion Development And By Demonstrating That Designs Reliably Meet The Specified Requirements Over The Operational Envelope Before The First Flight. The Development Of Advanced Ground Test Technology Components And Systems That Are Capable Of Enhancing Environment Simulation, Minimizing Program Test Time, Cost And Risk And Meeting Environmental And Safety Regulations Is Focused On Near-Term Products That Augment Existing State-Of-The-Art Propulsion System Test Facilities. Thus Improved Capabilities To Model And Predict Component Behavior In Harsh Ground Test Environments Are Needed For Enhanced Facility Design. In Particular, Components Such As Pumps, Turbines, Valves And Chokes May Experience Vibration And Damage Due To Cavitation In The Flowing Liquid, And Any Reduction In The Severity Of The Operating Conditions Would Provide Expanded Test And Performance Benefits. The Proposed Innovation Is To Develop An Unsteady Cavitation Model Based On A Tabular Equation Of State And A Representation Of Cavitation Bubble Dynamics That Together Describe The Growth And Collapse Of Nucleated Bubbles In A Liquid Cryogen. Important Nonequilibrium Mechanical And Thermal Effects Will Be Considered By Using A Drift-Flux Model And Adding An Additional Energy Equation For The Liquid Temperature. Validation Of The Advanced Cavitation Models Will Be Accomplished For Both Steady And Unsteady Flows By Comparing Surface Pressure And Temperature Data And Computing Power Spectra From Frequency Domain Analyses. The Final Analysis Tool Will Be Used To Demonstrate The Significant Nonequilibrium Flow Behavior For Both The Validation Cases And Actual Production Analysis Problems Of Interest To Nasa.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $750,000.00
- National Aeronautics And Space Administration (Nasa)
- FA865015C2513
- Numerical Analysis For Scramjet And Cold Start
- 5 Sep 2018
- Numerical Analysis For Scramjet And Cold Start
- Fa8650 Usaf Afmc Afrl/Rqk
- Department Of Defense (Dod)
- $477,059.00
- Department Of Defense (Dod)
- FA865019P2027
- Sbir Phase I, Liquid Injection Modeling For High Enthalpy Air Breathing Propulsion
- 29 Jan 2019
- Sbir Phase I, Liquid Injection Modeling For High Enthalpy Air Breathing Propulsion
- Fa8650 Usaf Afmc Afrl Pzl Rak Rxk
- Department Of Defense (Dod)
- $149,992.00
- Department Of Defense (Dod)
- FA865015C2513
- Q1ee Tetra Res's Num Analys For Scramj&Cold Start
- 14 Jun 2019
- Q1ee Tetra Res's Num Analys For Scramj&Cold Start
- Fa8650 Usaf Afmc Afrl Pzl Rak Rxk
- Department Of Defense (Dod)
- $556,164.00
- Department Of Defense (Dod)