Plasma Controls, Llc
Dba Plasma Controls Llc
CAGE Code: 4YGX5
NCAGE Code: 4YGX5
Status: Active
Type: Commercial Supplier
Dun & Bradstreet (DUNS): 809071538
Summary
Plasma Controls, Llc, Dba Plasma Controls Llc is an Active Commercial Supplier with the Cage Code 4YGX5 and is tracked by Dun & Bradstreet under DUNS Number 809071538..
Address
1180 La Eda Ln
Fort Collins CO 80526-4415
United States
Points of Contact
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Frequently Asked Questions (FAQ) for CAGE 4YGX5
- What is CAGE Code 4YGX5?
- 4YGX5 is the unique identifier used by NATO Organizations to reference the physical entity known as Plasma Controls, Llc Dba Plasma Controls Llc located at 1180 La Eda Ln, Fort Collins CO 80526-4415, United States.
- Who is CAGE Code 4YGX5?
- 4YGX5 refers to Plasma Controls, Llc Dba Plasma Controls Llc located at 1180 La Eda Ln, Fort Collins CO 80526-4415, United States.
- Where is CAGE Code 4YGX5 Located?
- CAGE Code 4YGX5 is located in Fort Collins, CO, USA.
Contracting History for CAGE 4YGX5 Most Recent 25 Records
- FA945322CA091
- Plasma Environment Simulator For Osam Operations
- 13 Jun 2022
- Plasma Environment Simulator For Osam Operations
- Fa9453 Afrl Rvk
- Department Of Defense (Dod)
- $240,404.00
- Department Of Defense (Dod)
- 80NSSC19C0546
- Energy And Velocity Analyzer For Distributions Of Electric Rockets
- 19 Aug 2019
- Energy And Velocity Analyzer For Distributions Of Electric Rockets
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $125,000.00
- National Aeronautics And Space Administration (Nasa)
- FA930019P1011
- Sbir I - Erosion Tolerant Snake Tongue Hollow Cathode
- 28 Mar 2019
- Sbir I - Erosion Tolerant Snake Tongue Hollow Cathode
- Fa9300 Aftc Pzr
- Department Of Defense (Dod)
- $150,000.00
- Department Of Defense (Dod)
- 80NSSC18P1765
- Ot - Testing And Analysis For The Beam Termperature Width Reduction Of Leeif Ion Source.
- 14 May 2018
- Ot - Testing And Analysis For The Beam Termperature Width Reduction Of Leeif Ion Source.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $13,000.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC23PB006
- Wien Filter Spectrometer (A.K.A. Exb Probe)
- 27 Apr 2023
- Wien Filter Spectrometer (A.K.A. Exb Probe)
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $12,843.00
- National Aeronautics And Space Administration (Nasa)
- FA940118P0031
- Heaterless Hollow Cathode System
- 1 May 2018
- Heaterless Hollow Cathode System
- Fa9401 377 Msg Pk
- Department Of Defense (Dod)
- $56,000.00
- Department Of Defense (Dod)
- 80NSSC18P3153
- Electrostatic Analyzers For Hall Effect Thruster
- 22 Aug 2018
- Electrostatic Analyzers For Hall Effect Thruster
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $34,977.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18C0108
- Plasma Controls, Llc Will Develop An Iodine-Compatible Hollow Cathode For Use In Hall-Effect Thrusters. Materials In Current State-Of-The-Art Electron Emitters, And Many Of The Materials Used In Mounting Hardware, Are Not Compatible In A High-Temperature Iodine Environment. This Includes Cathodes That Use Inserts Made From Porous Tungsten Impregnated With Ceramics Containing Barium Oxide, Which Can Be Susceptible To Rapid Decomposition Of The Ceramic By Iodine, And Lanthanum Hexaboride-Based Inserts, Which Are Subject To Rapid Surface Decomposition By Iodine. The Work Function Of Both Types Of Inserts Increases In The Presence Of Iodine, And The Temperature Of The Cathode Increases, Which Further Exacerbates The Decomposition Processes. We Will Use A Materials Science Based Approach To Evaluate The Chemical Interactions Between Iodine And A Range Of Potential Materials At Elevated Temperature. We Will Construct And Experimentally Test Candidate Cathodes In Relevant Iodine Environments To Identify Robust, Safe-To-Handle, Chemically-Stable Material Systems. In Phase Ii Work, We Will (1) Perform Long Duration Wear Tests To Demonstrate Adequately Long Lifetime Capability And (2) Integrate The Cathodes Into Iodine Storage, Feed, And Thruster Systems Through Industry And Government Partnerships.
- 25 Mar 2020
- Plasma Controls, Llc Will Develop An Iodine-Compatible Hollow Cathode For Use In Hall-Effect Thrusters. Materials In Current State-Of-The-Art Electron Emitters, And Many Of The Materials Used In Mounting Hardware, Are Not Compatible In A High-Temperature Iodine Environment. This Includes Cathodes That Use Inserts Made From Porous Tungsten Impregnated With Ceramics Containing Barium Oxide, Which Can Be Susceptible To Rapid Decomposition Of The Ceramic By Iodine, And Lanthanum Hexaboride-Based Inserts, Which Are Subject To Rapid Surface Decomposition By Iodine. The Work Function Of Both Types Of Inserts Increases In The Presence Of Iodine, And The Temperature Of The Cathode Increases, Which Further Exacerbates The Decomposition Processes. We Will Use A Materials Science Based Approach To Evaluate The Chemical Interactions Between Iodine And A Range Of Potential Materials At Elevated Temperature. We Will Construct And Experimentally Test Candidate Cathodes In Relevant Iodine Environments To Identify Robust, Safe-To-Handle, Chemically-Stable Material Systems. In Phase Ii Work, We Will (1) Perform Long Duration Wear Tests To Demonstrate Adequately Long Lifetime Capability And (2) Integrate The Cathodes Into Iodine Storage, Feed, And Thruster Systems Through Industry And Government Partnerships.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $750,000.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18C0108
- Plasma Controls, Llc Will Develop An Iodine-Compatible Hollow Cathode For Use In Hall-Effect Thrusters. Materials In Current State-Of-The-Art Electron Emitters, And Many Of The Materials Used In Mounting Hardware, Are Not Compatible In A High-Temperature Iodine Environment. This Includes Cathodes That Use Inserts Made From Porous Tungsten Impregnated With Ceramics Containing Barium Oxide, Which Can Be Susceptible To Rapid Decomposition Of The Ceramic By Iodine, And Lanthanum Hexaboride-Based Inserts, Which Are Subject To Rapid Surface Decomposition By Iodine. The Work Function Of Both Types Of Inserts Increases In The Presence Of Iodine, And The Temperature Of The Cathode Increases, Which Further Exacerbates The Decomposition Processes. We Will Use A Materials Science Based Approach To Evaluate The Chemical Interactions Between Iodine And A Range Of Potential Materials At Elevated Temperature. We Will Construct And Experimentally Test Candidate Cathodes In Relevant Iodine Environments To Identify Robust, Safe-To-Handle, Chemically-Stable Material Systems. In Phase Ii Work, We Will (1) Perform Long Duration Wear Tests To Demonstrate Adequately Long Lifetime Capability And (2) Integrate The Cathodes Into Iodine Storage, Feed, And Thruster Systems Through Industry And Government Partnerships.
- 2 May 2018
- Plasma Controls, Llc Will Develop An Iodine-Compatible Hollow Cathode For Use In Hall-Effect Thrusters. Materials In Current State-Of-The-Art Electron Emitters, And Many Of The Materials Used In Mounting Hardware, Are Not Compatible In A High-Temperature Iodine Environment. This Includes Cathodes That Use Inserts Made From Porous Tungsten Impregnated With Ceramics Containing Barium Oxide, Which Can Be Susceptible To Rapid Decomposition Of The Ceramic By Iodine, And Lanthanum Hexaboride-Based Inserts, Which Are Subject To Rapid Surface Decomposition By Iodine. The Work Function Of Both Types Of Inserts Increases In The Presence Of Iodine, And The Temperature Of The Cathode Increases, Which Further Exacerbates The Decomposition Processes. We Will Use A Materials Science Based Approach To Evaluate The Chemical Interactions Between Iodine And A Range Of Potential Materials At Elevated Temperature. We Will Construct And Experimentally Test Candidate Cathodes In Relevant Iodine Environments To Identify Robust, Safe-To-Handle, Chemically-Stable Material Systems. In Phase Ii Work, We Will (1) Perform Long Duration Wear Tests To Demonstrate Adequately Long Lifetime Capability And (2) Integrate The Cathodes Into Iodine Storage, Feed, And Thruster Systems Through Industry And Government Partnerships.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $750,000.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18C0108
- Plasma Controls, Llc Will Develop An Iodine-Compatible Hollow Cathode For Use In Hall-Effect Thrusters. Materials In Current State-Of-The-Art Electron Emitters, And Many Of The Materials Used In Mounting Hardware, Are Not Compatible In A High-Temperature Iodine Environment. This Includes Cathodes That Use Inserts Made From Porous Tungsten Impregnated With Ceramics Containing Barium Oxide, Which Can Be Susceptible To Rapid Decomposition Of The Ceramic By Iodine, And Lanthanum Hexaboride-Based Inserts, Which Are Subject To Rapid Surface Decomposition By Iodine. The Work Function Of Both Types Of Inserts Increases In The Presence Of Iodine, And The Temperature Of The Cathode Increases, Which Further Exacerbates The Decomposition Processes. We Will Use A Materials Science Based Approach To Evaluate The Chemical Interactions Between Iodine And A Range Of Potential Materials At Elevated Temperature. We Will Construct And Experimentally Test Candidate Cathodes In Relevant Iodine Environments To Identify Robust, Safe-To-Handle, Chemically-Stable Material Systems. In Phase Ii Work, We Will (1) Perform Long Duration Wear Tests To Demonstrate Adequately Long Lifetime Capability And (2) Integrate The Cathodes Into Iodine Storage, Feed, And Thruster Systems Through Industry And Government Partnerships.
- 4 Jun 2018
- Plasma Controls, Llc Will Develop An Iodine-Compatible Hollow Cathode For Use In Hall-Effect Thrusters. Materials In Current State-Of-The-Art Electron Emitters, And Many Of The Materials Used In Mounting Hardware, Are Not Compatible In A High-Temperature Iodine Environment. This Includes Cathodes That Use Inserts Made From Porous Tungsten Impregnated With Ceramics Containing Barium Oxide, Which Can Be Susceptible To Rapid Decomposition Of The Ceramic By Iodine, And Lanthanum Hexaboride-Based Inserts, Which Are Subject To Rapid Surface Decomposition By Iodine. The Work Function Of Both Types Of Inserts Increases In The Presence Of Iodine, And The Temperature Of The Cathode Increases, Which Further Exacerbates The Decomposition Processes. We Will Use A Materials Science Based Approach To Evaluate The Chemical Interactions Between Iodine And A Range Of Potential Materials At Elevated Temperature. We Will Construct And Experimentally Test Candidate Cathodes In Relevant Iodine Environments To Identify Robust, Safe-To-Handle, Chemically-Stable Material Systems. In Phase Ii Work, We Will (1) Perform Long Duration Wear Tests To Demonstrate Adequately Long Lifetime Capability And (2) Integrate The Cathodes Into Iodine Storage, Feed, And Thruster Systems Through Industry And Government Partnerships.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $750,000.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21P0631
- Exb Probe (Wein Filter) & Cable Set
- 17 Dec 2020
- Exb Probe (Wein Filter) & Cable Set
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $12,643.00
- National Aeronautics And Space Administration (Nasa)