Tao Of Systems Integration, Inc.
Dba Tao Of Systems Integration Inc
CAGE Code: 02SS7
NCAGE Code: 02SS7
Status: Active
Type: Commercial Supplier
Dun & Bradstreet (DUNS): 840701445
Summary
Tao Of Systems Integration, Inc., Dba Tao Of Systems Integration Inc is an Active Commercial Supplier with the Cage Code 02SS7 and is tracked by Dun & Bradstreet under DUNS Number 840701445..
Address
1100 Exploration Way
Hampton VA 23666-6264
United States
Points of Contact
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Frequently Asked Questions (FAQ) for CAGE 02SS7
- What is CAGE Code 02SS7?
- 02SS7 is the unique identifier used by NATO Organizations to reference the physical entity known as Tao Of Systems Integration, Inc. Dba Tao Of Systems Integration Inc located at 1100 Exploration Way, Hampton VA 23666-6264, United States.
- Who is CAGE Code 02SS7?
- 02SS7 refers to Tao Of Systems Integration, Inc. Dba Tao Of Systems Integration Inc located at 1100 Exploration Way, Hampton VA 23666-6264, United States.
- Where is CAGE Code 02SS7 Located?
- CAGE Code 02SS7 is located in Hampton, VA, USA.
Contracting History for CAGE 02SS7 Most Recent 25 Records
- FA955018C0012
- Igf::Ot::Igf Sttr Phase Ii 24 Months
- 11 Sep 2018
- Igf::Ot::Igf Sttr Phase Ii 24 Months
- Fa9550 Afrl Afosr
- Department Of Defense (Dod)
- $749,839.00
- Department Of Defense (Dod)
- 80NSSC17P1075
- This Research Will Focus On Transonic Wind Tunnel Turbulence Measurements Sponsored By Wind Tunnel Characterization Working Group (Wtcwg). Hot Wire Anemometry Has Been The Typical Measurement Technique For Such Measurements. However, The Transonic Sensor Sensitivities Are Not Characteristic Of Low Speed Or Supersonic Environments. The Transonic Measurements Of Velocity, Density, Temperature, And Flow Angle That Make Up Free Stream Turbulence Will Require Simultaneous And Independent Measurements Using A Four Channel Anemometer System.
- 6 Apr 2018
- This Research Will Focus On Transonic Wind Tunnel Turbulence Measurements Sponsored By Wind Tunnel Characterization Working Group (Wtcwg). Hot Wire Anemometry Has Been The Typical Measurement Technique For Such Measurements. However, The Transonic Sensor Sensitivities Are Not Characteristic Of Low Speed Or Supersonic Environments. The Transonic Measurements Of Velocity, Density, Temperature, And Flow Angle That Make Up Free Stream Turbulence Will Require Simultaneous And Independent Measurements Using A Four Channel Anemometer System.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $27,865.00
- National Aeronautics And Space Administration (Nasa)
- FA955017P0004
- Igf::Ot::Igf (Sttr Phase I) Balloon-Based Disturbance Measurements In The Upper Atmosphere
- 28 Apr 2017
- Igf::Ot::Igf (Sttr Phase I) Balloon-Based Disturbance Measurements In The Upper Atmosphere
- Fa9550 Afrl Afosr
- Department Of Defense (Dod)
- $149,981.00
- Department Of Defense (Dod)
- 80NSSC19C0034
- Characterization Working Group (Wtcwg). Hot Wire Anemometry Has Been The Typical Measurement Technique For Such Measurements. However, The Transonic Sensor Sensitivities Are Not Characteristic Of Low Speed Or Supersonic Environments. The Transonic Measurements Of Velocity, Density, Temperature, And Flow Angle That Make Up Free Stream Turbulence Will Require Simultaneous And Independent Measurements Using A Four-Channel Anemometer System.
- 22 Mar 2019
- Characterization Working Group (Wtcwg). Hot Wire Anemometry Has Been The Typical Measurement Technique For Such Measurements. However, The Transonic Sensor Sensitivities Are Not Characteristic Of Low Speed Or Supersonic Environments. The Transonic Measurements Of Velocity, Density, Temperature, And Flow Angle That Make Up Free Stream Turbulence Will Require Simultaneous And Independent Measurements Using A Four-Channel Anemometer System.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $17,366.00
- National Aeronautics And Space Administration (Nasa)
- NND10AK16C
- Hot Film Work For Gulfstream Iii Subsonic Research Aircraft
- 13 Oct 2011
- Hot Film Work For Gulfstream Iii Subsonic Research Aircraft
- Armstrong Flight Research Center
- National Aeronautics And Space Administration (Nasa)
- $253,943.00
- National Aeronautics And Space Administration (Nasa)