Connecticut Analytical Corporation
Dba Connecticut Analytical Corp

CAGE Code: 1T4H0

NCAGE Code: 1T4H0

Status: Active

Type: Manufacturer

Dun & Bradstreet (DUNS): 783630189

Summary

Connecticut Analytical Corporation, Dba Connecticut Analytical Corp is an Active Manufacturer with the Cage Code 1T4H0 and is tracked by Dun & Bradstreet under DUNS Number 783630189..

Address

696 Amity Rd
Bethany CT 06524-3006
United States

Points of Contact

No Points of Contact...

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CAGE Code FAQ Frequently Asked Questions (FAQ) for CAGE 1T4H0

What is CAGE Code 1T4H0?
1T4H0 is the unique identifier used by NATO Organizations to reference the physical entity known as Connecticut Analytical Corporation Dba Connecticut Analytical Corp located at 696 Amity Rd, Bethany CT 06524-3006, United States.
Who is CAGE Code 1T4H0?
1T4H0 refers to Connecticut Analytical Corporation Dba Connecticut Analytical Corp located at 696 Amity Rd, Bethany CT 06524-3006, United States.
Where is CAGE Code 1T4H0 Located?
CAGE Code 1T4H0 is located in Bethany, CT, USA.

Contracting History for CAGE 1T4H0 Contracting History for CAGE 1T4H0 Most Recent 25 Records

W5170123C0104
Bi-Monthly Status Report
3 Apr 2023
W27p Usa Acq Spt Ctr
Department Of Defense (Dod)
$248,541.58
80NSSC19C0188
In-Situ Electrospray Capture Of Organic Bearing Particulates From Alien Water Fountains
24 Feb 2021
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$748,693.00
80NSSC19C0188
In-Situ Electrospray Capture Of Organic Bearing Particulates From Alien Water Fountains
12 Nov 2021
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$748,693.00
80NSSC19C0188
In-Situ Electrospray Capture Of Organic Bearing Particulates From Alien Water Fountains
8 Jun 2021
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$748,693.00
80NSSC19C0188
In-Situ Electrospray Capture Of Organic Bearing Particulates From Alien Water Fountains
6 Aug 2021
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$748,693.00
80NSSC19C0188
In-Situ Electrospray Capture Of Organic Bearing Particulates From Alien Water Fountains
14 Aug 2019
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$748,693.00
80NSSC19C0188
Eo14042 In-Situ Electrospray Capture Of Organic Bearing Particulates From Alien Water Fountains
13 Oct 2021
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$748,693.00
80NSSC19C0158
Eo14042 In-Situ Electrospray Capture Of Organic Bearing Particulates From Comets And Celestial Bodies
15 Feb 2022
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$733,262.00
80NSSC19C0158
In-Situ Electrospray Capture Of Organic Bearing Particulates From Comets And Celestial Bodies
14 Aug 2019
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$733,262.00
80NSSC19C0158
In-Situ Electrospray Capture Of Organic Bearing Particulates From Comets And Celestial Bodies
6 Aug 2021
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$733,262.00
80NSSC19C0158
In-Situ Electrospray Capture Of Organic Bearing Particulates From Comets And Celestial Bodies
27 Jan 2021
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$733,262.00
80NSSC19C0158
In-Situ Electrospray Capture Of Organic Bearing Particulates From Comets And Celestial Bodies
15 Nov 2021
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$733,262.00
80NSSC19C0158
Eo14042 In-Situ Electrospray Capture Of Organic Bearing Particulates From Comets And Celestial Bodies
14 Oct 2021
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$733,262.00
80NSSC18P2095
Nasa Has Need For Technologies That Can Enable Sampling From Water Jets, Such As Those Observed Emanating From The Moon Enceladus And From The Moon Europa. We Propose To Leverage Past Observations Of The Ability Of Electrospray Ionization To Capture And Concentrate Polar Or Polarizable Trace Species Without Damage, And Combine That Knowledge With Recent Discoveries In Developing A Hypervelocity Ice-Gun For Nasa Studies Aimed At Ice Grain Capture Simulations. The Phase I Effort Will Focus On Using The Ice Gun We Created Under Prior Nasa Support, And Add A Cold Plasma Curtain To Pre-Charge An Incident Ice Grain, And Then Add A Novel Electrospray Element That We Believe Will Enable In-Situ Organic Analysis Capability Previously Unattainable On Board A Spacecraft Using Existing Nasa Mass Spectrometer Hardware. Incident Ice Grain Impacts Into Aerogel Create A Rearward Plume Of Water Vapor That May Contain A High Percentage Of Trace Organic Species. Using A Cross-Current Electrospray Source, These Species May Be Charged To Form Multiply Charged Ions Capable Of Being Interrogated In-Situ Using A Mass Analyzer, While Preserving Aerogel Impact Samples For A Return Mission. This Proposal Endeavors To Address One Of The Major Concerns In Any Particulate Impact-Capture Mission, Is The Potential Loss Of Valuable Samples Entrained In Aerogel. In Addition, The Long Flight Time Back To Earth Results In Significant Potential Discovery Delays. With The Proposed Technology, Nasa Can Now Perform In-Situ Organic Analysis Of Incident Ice Grains In Near Real-Time, And Have Impact Samples Retained For A Return Mission For Additional Study On Earth.
23 Jul 2018
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$124,562.00
80NSSC18P2034
Nasa Has Need For Technologies That Can Enable Sampling From Asteroids And From Depth In A Comet Nucleus, Improved In-Situ Analysis Of Comets. It Has Been Identified That There Is Also A Requirement For Improved Dust Environment Measurements&Particle Analysis, Small Body Resource Identification, And/Or Quantification Of Potential Small Body Resources (E.G., Oxygen, Water And Other Volatiles, Hydrated Minerals, Carbon Compounds, Fuels, Etc.). We Propose To Leverage Past Observations Of The Ability Of Electrospray Ionization To Capture And Concentrate Polar Or Polarizable Trace Species Without Damage, And Combine That Knowledge With Recent Discoveries In Developing A Hyper Velocity Ice-Gun For Nasa Studies Aimed At Ice Grain Capture Simulations. The Phase I Effort Will Focus On Using The Ice Gun We Created Under Prior Nasa Support, And Add A Novel Electrospray Cross-Current Element That Creates A Soft Charging Plume Across A Series Of Discrete Deceleration Aerogel Plates That We Believe Will Enable In-Situ Organic Analysis Capability Previously Unattainable On Board A Spacecraft Using Existing Nasa Mass Spectrometer Hardware.
12 Feb 2019
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$111,999.00
80NSSC19C0247
The Proposed Concept Offers A Potential For Game-Changing New Technology That May Obviate A Turbo Pump In Many Applications While Promising To Provide Significant Cost Savings With Unprecedented Reliability And Longevity For Future Space Missions.
19 Aug 2019
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$124,436.00
80NSSC18C0056
E014042 This Proposal Evolved As A Result Of A Conversation With A Nasa Scientist Regarding Plans For A Mission To One Of Several Icy Moons In The Solar System To Seek Signs Of Life Based On Observed Water Plume Emissions. In Preparation For Such A Mission, Spacecraft Will Have To Pass Through Clouds Of Ice Particulates, Which Will Pose Challanges In Organic Species Collection, And Possible Damage To Instruments. Accordingly, There Is A Need For Simulating The Production Of Hyper Velocity Ice In The Size Range Of 50Nm Through 2 Microns. The Nasa Ames Vertical Gun Range Was Designed To Propell Solid Projectiles For Studying The Effects Of Meteorite Impacts On Celestial Bodies And Potential Micro-Meteoroid Damage To Spacecraft. At The Far End Of The Barrel, A Gunpowder Explosion Is Used To Compress Hydrogen Gas To As Much As 1 Million Times Atmospheric Pressure, Firing A Projectile Pellet At Speeds Between 7,000 And 15,000 Mph . This Approach Is Not Suitable For Ice Particles, So We Have Developed A Novel Ice Gun Using Electrosprays That Can Achieve A Hyper Velocity Net Result Without Damage To The Sample Grain.
12 Nov 2021
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$749,019.00
W31P4Q13C0073
Igf::Ot::Igf
3 Feb 2017
W6qk Acc-Rsa
Department Of Defense (Dod)
$1,944,080.24
80NSSC18C0056
This Proposal Evolved As A Result Of A Conversation With A Nasa Scientist Regarding Plans For A Mission To One Of Several Icy Moons In The Solar System To Seek Signs Of Life Based On Observed Water Plume Emissions. In Preparation For Such A Mission, Spacecraft Will Have To Pass Through Clouds Of Ice Particulates, Which Will Pose Challanges In Organic Species Collection, And Possible Damage To Instruments. Accordingly, There Is A Need For Simulating The Production Of Hyper Velocity Ice In The Size Range Of 50Nm Through 2 Microns. The Nasa Ames Vertical Gun Range Was Designed To Propell Solid Projectiles For Studying The Effects Of Meteorite Impacts On Celestial Bodies And Potential Micro-Meteoroid Damage To Spacecraft. At The Far End Of The Barrel, A Gunpowder Explosion Is Used To Compress Hydrogen Gas To As Much As 1 Million Times Atmospheric Pressure, Firing A Projectile Pellet At Speeds Between 7,000 And 15,000 Mph . This Approach Is Not Suitable For Ice Particles, So We Have Developed A Novel Ice Gun Using Electrosprays That Can Achieve A Hyper Velocity Net Result Without Damage To The Sample Grain.
17 Apr 2020
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$749,019.00
80NSSC18C0056
This Proposal Evolved As A Result Of A Conversation With A Nasa Scientist Regarding Plans For A Mission To One Of Several Icy Moons In The Solar System To Seek Signs Of Life Based On Observed Water Plume Emissions. In Preparation For Such A Mission, Spacecraft Will Have To Pass Through Clouds Of Ice Particulates, Which Will Pose Challanges In Organic Species Collection, And Possible Damage To Instruments. Accordingly, There Is A Need For Simulating The Production Of Hyper Velocity Ice In The Size Range Of 50Nm Through 2 Microns. The Nasa Ames Vertical Gun Range Was Designed To Propell Solid Projectiles For Studying The Effects Of Meteorite Impacts On Celestial Bodies And Potential Micro-Meteoroid Damage To Spacecraft. At The Far End Of The Barrel, A Gunpowder Explosion Is Used To Compress Hydrogen Gas To As Much As 1 Million Times Atmospheric Pressure, Firing A Projectile Pellet At Speeds Between 7,000 And 15,000 Mph . This Approach Is Not Suitable For Ice Particles, So We Have Developed A Novel Ice Gun Using Electrosprays That Can Achieve A Hyper Velocity Net Result Without Damage To The Sample Grain.
25 Aug 2021
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$749,019.00
80NSSC21C0151
Microbial Monitoring Of Spacecraft & Habitats Utilizing Advanced Metabolomics Analytical Methods
18 May 2021
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$123,243.00
80NSSC18C0056
This Proposal Evolved As A Result Of A Conversation With A Nasa Scientist Regarding Plans For A Mission To One Of Several Icy Moons In The Solar System To Seek Signs Of Life Based On Observed Water Plume Emissions. In Preparation For Such A Mission, Spacecraft Will Have To Pass Through Clouds Of Ice Particulates, Which Will Pose Challanges In Organic Species Collection, And Possible Damage To Instruments. Accordingly, There Is A Need For Simulating The Production Of Hyper Velocity Ice In The Size Range Of 50Nm Through 2 Microns. The Nasa Ames Vertical Gun Range Was Designed To Propell Solid Projectiles For Studying The Effects Of Meteorite Impacts On Celestial Bodies And Potential Micro-Meteoroid Damage To Spacecraft. At The Far End Of The Barrel, A Gunpowder Explosion Is Used To Compress Hydrogen Gas To As Much As 1 Million Times Atmospheric Pressure, Firing A Projectile Pellet At Speeds Between 7,000 And 15,000 Mph . This Approach Is Not Suitable For Ice Particles, So We Have Developed A Novel Ice Gun Using Electrosprays That Can Achieve A Hyper Velocity Net Result Without Damage To The Sample Grain.
8 Feb 2021
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$749,019.00
W31P4Q13C0073
Darpa Small Business Innovation Research (Sbir) Phase Ii Program For Effort Entitled,"Improved Dried Biological Specimen Materials, Recovery And Processing For Diagnostics."
4 Apr 2019
W6qk Acc-Rsa
Department Of Defense (Dod)
$1,942,965.26
80NSSC18P2095
Nasa Has Need For Technologies That Can Enable Sampling From Water Jets, Such As Those Observed Emanating From The Moon Enceladus And From The Moon Europa. We Propose To Leverage Past Observations Of The Ability Of Electrospray Ionization To Capture And Concentrate Polar Or Polarizable Trace Species Without Damage, And Combine That Knowledge With Recent Discoveries In Developing A Hypervelocity Ice-Gun For Nasa Studies Aimed At Ice Grain Capture Simulations. The Phase I Effort Will Focus On Using The Ice Gun We Created Under Prior Nasa Support, And Add A Cold Plasma Curtain To Pre-Charge An Incident Ice Grain, And Then Add A Novel Electrospray Element That We Believe Will Enable In-Situ Organic Analysis Capability Previously Unattainable On Board A Spacecraft Using Existing Nasa Mass Spectrometer Hardware. Incident Ice Grain Impacts Into Aerogel Create A Rearward Plume Of Water Vapor That May Contain A High Percentage Of Trace Organic Species. Using A Cross-Current Electrospray Source, These Species May Be Charged To Form Multiply Charged Ions Capable Of Being Interrogated In-Situ Using A Mass Analyzer, While Preserving Aerogel Impact Samples For A Return Mission. This Proposal Endeavors To Address One Of The Major Concerns In Any Particulate Impact-Capture Mission, Is The Potential Loss Of Valuable Samples Entrained In Aerogel. In Addition, The Long Flight Time Back To Earth Results In Significant Potential Discovery Delays. With The Proposed Technology, Nasa Can Now Perform In-Situ Organic Analysis Of Incident Ice Grains In Near Real-Time, And Have Impact Samples Retained For A Return Mission For Additional Study On Earth.
13 Feb 2019
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$124,562.00
80NSSC18C0056
Eo14042 This Proposal Evolved As A Result Of A Conversation With A Nasa Scientist Regarding Plans For A Mission To One Of Several Icy Moons In The Solar System To Seek Signs Of Life Based On Observed Water Plume Emissions. In Preparation For Such A Mission, Spacecraft Will Have To Pass Through Clouds Of Ice Particulates, Which Will Pose Challanges In Organic Species Collection, And Possible Damage To Instruments. Accordingly, There Is A Need For Simulating The Production Of Hyper Velocity Ice In The Size Range Of 50Nm Through 2 Microns. The Nasa Ames Vertical Gun Range Was Designed To Propell Solid Projectiles For Studying The Effects Of Meteorite Impacts On Celestial Bodies And Potential Micro-Meteoroid Damage To Spacecraft. At The Far End Of The Barrel, A Gunpowder Explosion Is Used To Compress Hydrogen Gas To As Much As 1 Million Times Atmospheric Pressure, Firing A Projectile Pellet At Speeds Between 7,000 And 15,000 Mph . This Approach Is Not Suitable For Ice Particles, So We Have Developed A Novel Ice Gun Using Electrosprays That Can Achieve A Hyper Velocity Net Result Without Damage To The Sample Grain.
21 Dec 2021
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$749,019.00