Research In Flight Llc
Dba Research In Flight
Div Research In Flight
CAGE Code: 7DVS1
NCAGE Code: 7DVS1
Status: Active
Type: Commercial Supplier
Summary
Research In Flight Llc, Dba Research In Flight, Div Research In Flight is an Active Commercial Supplier with the Cage Code 7DVS1.
Address
1919 N Ashe Ct
Auburn AL 36830-2691
United States
Points of Contact
No Points of Contact...
Related Information
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Frequently Asked Questions (FAQ) for CAGE 7DVS1
- What is CAGE Code 7DVS1?
- 7DVS1 is the unique identifier used by NATO Organizations to reference the physical entity known as Research In Flight Llc Dba Research In Flight Div Research In Flight located at 1919 N Ashe Ct, Auburn AL 36830-2691, United States.
- Who is CAGE Code 7DVS1?
- 7DVS1 refers to Research In Flight Llc Dba Research In Flight Div Research In Flight located at 1919 N Ashe Ct, Auburn AL 36830-2691, United States.
- Where is CAGE Code 7DVS1 Located?
- CAGE Code 7DVS1 is located in Auburn, AL, USA.
Contracting History for CAGE 7DVS1 Most Recent 25 Records
- FA864923P1213
- Sttr Phase Ii Proposal F2-16278 - A Rapid Aerodynamic Prediction Tool For Maneuvering Hypersonic Air Vehicles
- 21 Sep 2023
- Sttr Phase Ii Proposal F2-16278 - A Rapid Aerodynamic Prediction Tool For Maneuvering Hypersonic Air Vehicles
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $1,226,789.00
- Department Of Defense (Dod)
- FA864923P0924
- Accelerated Preconditioned Reynolds Averaged Navier Stokes Simulations For Hypersonic Flight Vehicles
- 4 May 2023
- Accelerated Preconditioned Reynolds Averaged Navier Stokes Simulations For Hypersonic Flight Vehicles
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $75,000.00
- Department Of Defense (Dod)
- FA864923P0927
- Real-Time Assessment Of Battle Damage On Air Vehicle Mission Profiles
- 4 May 2023
- Real-Time Assessment Of Battle Damage On Air Vehicle Mission Profiles
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $75,000.00
- Department Of Defense (Dod)
- FA864923P0441
- Multi-Fidelity Supersonic Flow Solver For Preliminary Design & Optimization
- 8 Feb 2023
- Multi-Fidelity Supersonic Flow Solver For Preliminary Design & Optimization
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $1,248,744.00
- Department Of Defense (Dod)
- FA864923P0368
- A Rapid Aerodynamic Prediction Tool For Maneuvering Hypersonic Air Vehicles
- 4 Nov 2022
- A Rapid Aerodynamic Prediction Tool For Maneuvering Hypersonic Air Vehicles
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $75,000.00
- Department Of Defense (Dod)
- FA864923P0369
- Comprehensive Acoustics Characterization Framework For Electric Vertical Takeoff And Landing Vehicle/High-Speed Vertical Take-Off And Landing (Evtol/Hsvtol) Aircraft
- 4 Nov 2022
- Comprehensive Acoustics Characterization Framework For Electric Vertical Takeoff And Landing Vehicle/High-Speed Vertical Take-Off And Landing (Evtol/Hsvtol) Aircraft
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $75,000.00
- Department Of Defense (Dod)
- FA864922P0081
- A Multi-Fidelity Supersonic Flow Solver For Preliminary Design & Optimization
- 3 Nov 2021
- A Multi-Fidelity Supersonic Flow Solver For Preliminary Design & Optimization
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $50,000.00
- Department Of Defense (Dod)
- FA864921P0182
- Electric Scalable Aerial Transport
- 10 Feb 2021
- Electric Scalable Aerial Transport
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $150,000.00
- Department Of Defense (Dod)
- FA864921P0162
- Improvement Of Multi-Rotor Aerial Vehicles Performance Using Reduced-Order Aero-Mechanical Models
- 21 Jan 2021
- Improvement Of Multi-Rotor Aerial Vehicles Performance Using Reduced-Order Aero-Mechanical Models
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $150,000.00
- Department Of Defense (Dod)
- FA864921P0213
- Electric Extended Range Airship With Modular Payload
- 12 Feb 2021
- Electric Extended Range Airship With Modular Payload
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $150,000.00
- Department Of Defense (Dod)
- 80NSSC21C0025
- Eo14042 Air Vehicle Gust Response Analysis For Conceptual Design
- 10 Jan 2023
- Eo14042 Air Vehicle Gust Response Analysis For Conceptual Design
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,999.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0025
- Air Vehicle Gust Response Analysis For Conceptual Design
- 17 Feb 2023
- Air Vehicle Gust Response Analysis For Conceptual Design
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,999.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0025
- Air Vehicle Gust Response Analysis For Conceptual Design
- 26 Jan 2021
- Air Vehicle Gust Response Analysis For Conceptual Design
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,999.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC20C0586
- Early-Design Aeroacoustics Prediction For Distributed Electric Propulsion Vehicles Using Flightstream
- 11 Feb 2021
- Early-Design Aeroacoustics Prediction For Distributed Electric Propulsion Vehicles Using Flightstream
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,988.00
- National Aeronautics And Space Administration (Nasa)
- 80LARC19C0013
- Nasa Research Annoucement (Nra) For Moodular Generalized Framework For Assessing Aircraft Aero-Propulsive, Stability, And Control Characteristics Nasa Continues To Investigate The Potential Of Advanced, Innovative Propulsion And Airframe Concepts To Improve Efficiency For Fuel And Noise Reduction And To Enable New Visions For Flexible, On-Demand Travel For The Public. The Potential Benefits Of Advanced Vehicle Designs Such As Blended Wing Bodies And Distributed Electric Propulsion Have Long Been Known, But These Designs Have Been Slow To Transition Into The Commercial And Public Domain Because Of Gaps In The Ability To Efficiently And Reliably Model Them In The Design Tool Sets. Modeling These Designs Is Particularly Challenging For The Conceptual Design Phase Where Mission Targets And Performance Goals Are First Translated Into Potential Aircraft Designs That Can Meet Those Goals. However, Conceptual Design And Analysis Of Unconventional Airframe (Geometries That Differ From The Historically Popular Wing-And-Tube Design Or Which Take Advantage Of Flow Augmentation To Improve Lift/Drag Characteristics) And Unconventional Propulsion (Energy From Sources Other Than Carbon Liquid Fuel) Concepts And Technologies Are Currently Used Within Nasa For Technology Portfolio Investment Planning, Development Of Advanced Concepts To Provide Technology Pull, And Independent Technical Assessment Of New Concepts. Nasa S Systems Analysts Need Improved Conceptual Design And Analysis Tools To Support These Efforts. Many Traditional Methods Of Sizing Aircraft Control Surfaces And Assuring Acceptable Handling Qualities Have Lost Their Validity As More Unconventional Aircraft Are Being Studied, And Additional Dynamic Modes Might Become Unstable. Nasa Is Seeking To Develop Methods For Analysis Of Aircraft Static And Dynamic Stability Characteristics Suitable For Unconventional Aircraft In The Conceptual Design Stage. The Methods Should Be Verified And Demonstrated Through Simulation Of The Dynamics Of Unconventional Fixed-Wing Aircraft Configurations With Tight Coupling Of Propulsion And Aerodynamics Characteristics, Including Evaluation Of Active Control Systems To Enable Design Of Unconventional Aircraft. This Statement Of Work Is The Result Of A Proposal Submitted By Research In Flight, Llc For Award Under The Nasa Headquarters Armd Nasa Research Announcement (Nra) Entitled Research Opportunities In Aeronautics 2018, Amendment Nnh18zea001n, Subtopic 2.1.6. The Contractor Shall Develop Tools, Processes, And Methods That Allow The Conceptual Designer Or Analyst To Assess And Evaluate The Stability And Control Characteristics Of Unconventional Aircraft Configurations.
- 6 Dec 2021
- Nasa Research Annoucement (Nra) For Moodular Generalized Framework For Assessing Aircraft Aero-Propulsive, Stability, And Control Characteristics Nasa Continues To Investigate The Potential Of Advanced, Innovative Propulsion And Airframe Concepts To Improve Efficiency For Fuel And Noise Reduction And To Enable New Visions For Flexible, On-Demand Travel For The Public. The Potential Benefits Of Advanced Vehicle Designs Such As Blended Wing Bodies And Distributed Electric Propulsion Have Long Been Known, But These Designs Have Been Slow To Transition Into The Commercial And Public Domain Because Of Gaps In The Ability To Efficiently And Reliably Model Them In The Design Tool Sets. Modeling These Designs Is Particularly Challenging For The Conceptual Design Phase Where Mission Targets And Performance Goals Are First Translated Into Potential Aircraft Designs That Can Meet Those Goals. However, Conceptual Design And Analysis Of Unconventional Airframe (Geometries That Differ From The Historically Popular Wing-And-Tube Design Or Which Take Advantage Of Flow Augmentation To Improve Lift/Drag Characteristics) And Unconventional Propulsion (Energy From Sources Other Than Carbon Liquid Fuel) Concepts And Technologies Are Currently Used Within Nasa For Technology Portfolio Investment Planning, Development Of Advanced Concepts To Provide Technology Pull, And Independent Technical Assessment Of New Concepts. Nasa S Systems Analysts Need Improved Conceptual Design And Analysis Tools To Support These Efforts. Many Traditional Methods Of Sizing Aircraft Control Surfaces And Assuring Acceptable Handling Qualities Have Lost Their Validity As More Unconventional Aircraft Are Being Studied, And Additional Dynamic Modes Might Become Unstable. Nasa Is Seeking To Develop Methods For Analysis Of Aircraft Static And Dynamic Stability Characteristics Suitable For Unconventional Aircraft In The Conceptual Design Stage. The Methods Should Be Verified And Demonstrated Through Simulation Of The Dynamics Of Unconventional Fixed-Wing Aircraft Configurations With Tight Coupling Of Propulsion And Aerodynamics Characteristics, Including Evaluation Of Active Control Systems To Enable Design Of Unconventional Aircraft. This Statement Of Work Is The Result Of A Proposal Submitted By Research In Flight, Llc For Award Under The Nasa Headquarters Armd Nasa Research Announcement (Nra) Entitled Research Opportunities In Aeronautics 2018, Amendment Nnh18zea001n, Subtopic 2.1.6. The Contractor Shall Develop Tools, Processes, And Methods That Allow The Conceptual Designer Or Analyst To Assess And Evaluate The Stability And Control Characteristics Of Unconventional Aircraft Configurations.
- Nasa Langley Research Center
- National Aeronautics And Space Administration (Nasa)
- $540,000.00
- National Aeronautics And Space Administration (Nasa)