Nanocomp Technologies, Inc.
CAGE Code: 32YC2
NCAGE Code: 32YC2
Status: Active
Type: Commercial Supplier
Dun & Bradstreet (DUNS): 169169443
Summary
Nanocomp Technologies, Inc. is an Active Commercial Supplier with the Cage Code 32YC2 and is tracked by Dun & Bradstreet under DUNS Number 169169443..
Address
57 Daniel Webster Hwy
Merrimack NH 03054-4811
United States
Points of Contact
Related Information
People who viewed this 'CAGE Code' also viewed...
Lightec Inc Nashua Corp Computer Products Div Global Knowledge Network North Country Wire Supply Total Quality Measures Inc Mouradian Quality Consulting Nashua Express M/A-Com Inc Eastern Pipe Service, Inc. Eptac Corp Reeds Ferry Lumber Corp Chem Fab Corp Merrimack Handling Equipment Corp Rfa Technology Associated Industrial Service Inc Associated Industrial Service Inc. Avnet Inc Mechanics Choice Div Marie Anaba Charles S. Cramer Ai Combat Systems Llc
Frequently Asked Questions (FAQ) for CAGE 32YC2
- What is CAGE Code 32YC2?
- 32YC2 is the unique identifier used by NATO Organizations to reference the physical entity known as Nanocomp Technologies, Inc. located at 57 Daniel Webster Hwy, Merrimack NH 03054-4811, United States.
- Who is CAGE Code 32YC2?
- 32YC2 refers to Nanocomp Technologies, Inc. located at 57 Daniel Webster Hwy, Merrimack NH 03054-4811, United States.
- Where is CAGE Code 32YC2 Located?
- CAGE Code 32YC2 is located in Merrimack, NH, USA.
Contracting History for CAGE 32YC2 Most Recent 25 Records
- 80NSSC21C0617
- Development Of High Strength Carbon Nanotube Yarn For Structural.Composites
- 20 Jul 2023
- Development Of High Strength Carbon Nanotube Yarn For Structural.Composites
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $5,806,923.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0617
- Development Of High Strength Carbon Nanotube Yarn For Structural.Composites
- 30 Sep 2021
- Development Of High Strength Carbon Nanotube Yarn For Structural.Composites
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $4,215,716.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0617
- Eo14042 Development Of High Strength Carbon Nanotube Yarn For Structural.Composites
- 9 Nov 2022
- Eo14042 Development Of High Strength Carbon Nanotube Yarn For Structural.Composites
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $4,215,716.00
- National Aeronautics And Space Administration (Nasa)
- 80LARC18C0007
- Development Of High Strength Carbon Nanotube Yarn For Structural Composites Structural Composites With Mechanical Properties That Are Multiple Times Those Of State-Of-The-Art (Soa) Carbon Fiber Reinforced Polymer Composites (Cfrp) Can Yield Significant Systems Level Benefits For Aerospace Vehicles. Carbon Nanotubes (Cnt) Have The Potential To Enable Mass Savings Due To Nanoscale Properties That Far Outperform Those Documented For Carbon Fibers However, Retaining Superior Nanoscale Properties In Bulk Has Been Challenging. Nasa Investments Under The Game Changing Development (Gcd) Program From 2012 - 2015 Yielded Improvements In Nanocomp Technologies Inc. S Cnt Material Characteristics That Produced Cnt Composites With Specific Strength And Specific Modulus Nearly Competitive With Unidirectional Carbon Fiber Composites Despite The Nanocomposite Being Far From Optimal. Over The Past Three Years, Nanocomp Technologies, Inc. Continued To Research And Develop The Manufacturing Parameters To The Point Where They Were Able To Realize An Approximate 50% Increase In Specific Tensile Strength Of The Yarn Over The Strength Attained At The End Of The Gcd Nanotechnology Project In 2015. The Cnt Yarn Strength Has Been Attained On An Experimental Scale And Shall Be Improved Further To Enable The Fabrication Of Cnt Composites With Strengths That Meet Nasa S Goals In Lightweight Structures. To Support This Application Of High Performance Cnt Material, The Material Formats Need To Be Available In Large Volumes With Consistent Quality To Permit The Processing Optimization Necessary To Produce Panel Level Composites With The Properties Being Sought. This Sbir Phase Iii Effort To Pursue Commercialization Objectives Resulting From The Previous Sbir Phase Iii Research And Development Activities, Including Cost Efficiencies In Production. The Technology Maturation Of The Carbon Nanotube (Cnt) Material, The Cnt Formats Delivered Will Be Evaluated For Nasa S Mission Needs In The Use Of Lightweight Aerospace Structures, Structural Components, And The Fabrication Of Prototype Aerospace Articles.
- 19 Sep 2022
- Development Of High Strength Carbon Nanotube Yarn For Structural Composites Structural Composites With Mechanical Properties That Are Multiple Times Those Of State-Of-The-Art (Soa) Carbon Fiber Reinforced Polymer Composites (Cfrp) Can Yield Significant Systems Level Benefits For Aerospace Vehicles. Carbon Nanotubes (Cnt) Have The Potential To Enable Mass Savings Due To Nanoscale Properties That Far Outperform Those Documented For Carbon Fibers However, Retaining Superior Nanoscale Properties In Bulk Has Been Challenging. Nasa Investments Under The Game Changing Development (Gcd) Program From 2012 - 2015 Yielded Improvements In Nanocomp Technologies Inc. S Cnt Material Characteristics That Produced Cnt Composites With Specific Strength And Specific Modulus Nearly Competitive With Unidirectional Carbon Fiber Composites Despite The Nanocomposite Being Far From Optimal. Over The Past Three Years, Nanocomp Technologies, Inc. Continued To Research And Develop The Manufacturing Parameters To The Point Where They Were Able To Realize An Approximate 50% Increase In Specific Tensile Strength Of The Yarn Over The Strength Attained At The End Of The Gcd Nanotechnology Project In 2015. The Cnt Yarn Strength Has Been Attained On An Experimental Scale And Shall Be Improved Further To Enable The Fabrication Of Cnt Composites With Strengths That Meet Nasa S Goals In Lightweight Structures. To Support This Application Of High Performance Cnt Material, The Material Formats Need To Be Available In Large Volumes With Consistent Quality To Permit The Processing Optimization Necessary To Produce Panel Level Composites With The Properties Being Sought. This Sbir Phase Iii Effort To Pursue Commercialization Objectives Resulting From The Previous Sbir Phase Iii Research And Development Activities, Including Cost Efficiencies In Production. The Technology Maturation Of The Carbon Nanotube (Cnt) Material, The Cnt Formats Delivered Will Be Evaluated For Nasa S Mission Needs In The Use Of Lightweight Aerospace Structures, Structural Components, And The Fabrication Of Prototype Aerospace Articles.
- Nasa Langley Research Center
- National Aeronautics And Space Administration (Nasa)
- $10,370,129.00
- National Aeronautics And Space Administration (Nasa)
- 80LARC18C0007
- Development Of High Strength Carbon Nanotube Yarn For Structural Composites Structural Composites With Mechanical Properties That Are Multiple Times Those Of State-Of-The-Art (Soa) Carbon Fiber Reinforced Polymer Composites (Cfrp) Can Yield Significant Systems Level Benefits For Aerospace Vehicles. Carbon Nanotubes (Cnt) Have The Potential To Enable Mass Savings Due To Nanoscale Properties That Far Outperform Those Documented For Carbon Fibers However, Retaining Superior Nanoscale Properties In Bulk Has Been Challenging. Nasa Investments Under The Game Changing Development (Gcd) Program From 2012 - 2015 Yielded Improvements In Nanocomp Technologies Inc. S Cnt Material Characteristics That Produced Cnt Composites With Specific Strength And Specific Modulus Nearly Competitive With Unidirectional Carbon Fiber Composites Despite The Nanocomposite Being Far From Optimal. Over The Past Three Years, Nanocomp Technologies, Inc. Continued To Research And Develop The Manufacturing Parameters To The Point Where They Were Able To Realize An Approximate 50% Increase In Specific Tensile Strength Of The Yarn Over The Strength Attained At The End Of The Gcd Nanotechnology Project In 2015. The Cnt Yarn Strength Has Been Attained On An Experimental Scale And Shall Be Improved Further To Enable The Fabrication Of Cnt Composites With Strengths That Meet Nasa S Goals In Lightweight Structures. To Support This Application Of High Performance Cnt Material, The Material Formats Need To Be Available In Large Volumes With Consistent Quality To Permit The Processing Optimization Necessary To Produce Panel Level Composites With The Properties Being Sought. This Sbir Phase Iii Effort To Pursue Commercialization Objectives Resulting From The Previous Sbir Phase Iii Research And Development Activities, Including Cost Efficiencies In Production. The Technology Maturation Of The Carbon Nanotube (Cnt) Material, The Cnt Formats Delivered Will Be Evaluated For Nasa S Mission Needs In The Use Of Lightweight Aerospace Structures, Structural Components, And The Fabrication Of Prototype Aerospace Articles.
- 27 Aug 2021
- Development Of High Strength Carbon Nanotube Yarn For Structural Composites Structural Composites With Mechanical Properties That Are Multiple Times Those Of State-Of-The-Art (Soa) Carbon Fiber Reinforced Polymer Composites (Cfrp) Can Yield Significant Systems Level Benefits For Aerospace Vehicles. Carbon Nanotubes (Cnt) Have The Potential To Enable Mass Savings Due To Nanoscale Properties That Far Outperform Those Documented For Carbon Fibers However, Retaining Superior Nanoscale Properties In Bulk Has Been Challenging. Nasa Investments Under The Game Changing Development (Gcd) Program From 2012 - 2015 Yielded Improvements In Nanocomp Technologies Inc. S Cnt Material Characteristics That Produced Cnt Composites With Specific Strength And Specific Modulus Nearly Competitive With Unidirectional Carbon Fiber Composites Despite The Nanocomposite Being Far From Optimal. Over The Past Three Years, Nanocomp Technologies, Inc. Continued To Research And Develop The Manufacturing Parameters To The Point Where They Were Able To Realize An Approximate 50% Increase In Specific Tensile Strength Of The Yarn Over The Strength Attained At The End Of The Gcd Nanotechnology Project In 2015. The Cnt Yarn Strength Has Been Attained On An Experimental Scale And Shall Be Improved Further To Enable The Fabrication Of Cnt Composites With Strengths That Meet Nasa S Goals In Lightweight Structures. To Support This Application Of High Performance Cnt Material, The Material Formats Need To Be Available In Large Volumes With Consistent Quality To Permit The Processing Optimization Necessary To Produce Panel Level Composites With The Properties Being Sought. This Sbir Phase Iii Effort To Pursue Commercialization Objectives Resulting From The Previous Sbir Phase Iii Research And Development Activities, Including Cost Efficiencies In Production. The Technology Maturation Of The Carbon Nanotube (Cnt) Material, The Cnt Formats Delivered Will Be Evaluated For Nasa S Mission Needs In The Use Of Lightweight Aerospace Structures, Structural Components, And The Fabrication Of Prototype Aerospace Articles.
- Nasa Langley Research Center
- National Aeronautics And Space Administration (Nasa)
- $10,370,129.00
- National Aeronautics And Space Administration (Nasa)