Supercool Metals Llc
CAGE Code: 74XP1
NCAGE Code: 74XP1
Status: Active
Type: Manufacturer
Summary
Supercool Metals Llc is an Active Manufacturer with the Cage Code 74XP1.
Address
21 Business Park Dr Ste 5B
Branford CT 06405-2935
United States
Points of Contact
No Points of Contact...
Related Information
No Related Information...
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Frequently Asked Questions (FAQ) for CAGE 74XP1
- What is CAGE Code 74XP1?
- 74XP1 is the unique identifier used by NATO Organizations to reference the physical entity known as Supercool Metals Llc located at 21 Business Park Dr Ste 5B, Branford CT 06405-2935, United States.
- Who is CAGE Code 74XP1?
- 74XP1 refers to Supercool Metals Llc located at 21 Business Park Dr Ste 5B, Branford CT 06405-2935, United States.
- Where is CAGE Code 74XP1 Located?
- CAGE Code 74XP1 is located in Branford, CT, USA.
Contracting History for CAGE 74XP1 Most Recent 25 Records
- FA864922P0817
- Superior Satellite Hinges With Bulk Metallic Glass Technology
- 7 Mar 2022
- Superior Satellite Hinges With Bulk Metallic Glass Technology
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $749,968.00
- Department Of Defense (Dod)
- FA864922P0817
- Superior Satellite Hinges With Bulk Metallic Glass Technology
- 17 May 2023
- Superior Satellite Hinges With Bulk Metallic Glass Technology
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $749,968.00
- Department Of Defense (Dod)
- SP470122C0057
- Supercool Metals Sbir Ii Proposal L2-0364 Entitled " Efficient Fabrication Of Components For Air And Space Systems Through Thermoplastic Forming Of Bulk Metallic Glasses"
- 16 Jun 2022
- Supercool Metals Sbir Ii Proposal L2-0364 Entitled " Efficient Fabrication Of Components For Air And Space Systems Through Thermoplastic Forming Of Bulk Metallic Glasses"
- Dcso Philadelphia
- Department Of Defense (Dod)
- $1,000,000.00
- Department Of Defense (Dod)
- FA864921P1109
- Superior Satellite Hinges With Bulk Metallic Glass Technology
- 3 May 2021
- Superior Satellite Hinges With Bulk Metallic Glass Technology
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $49,999.00
- Department Of Defense (Dod)
- FA865019C5093
- Development Of Bulk Metallic Glass For Spacecraft Applications Using Thermoplastic Forming
- 10 May 2019
- Development Of Bulk Metallic Glass For Spacecraft Applications Using Thermoplastic Forming
- Fa8650 Usaf Afmc Afrl Pzl Afrl/Pzl
- Department Of Defense (Dod)
- $749,988.00
- Department Of Defense (Dod)
- FA865019C5093
- Development Of Bulk Metallic Glass For Spacecraft Applications Using Thermoplastic Forming
- 28 Jun 2021
- Development Of Bulk Metallic Glass For Spacecraft Applications Using Thermoplastic Forming
- Fa8650 Usaf Afmc Afrl Pzl Rak Rxk
- Department Of Defense (Dod)
- $749,988.00
- Department Of Defense (Dod)
- 80NSSC18C0132
- E014042 Demand For Novel Manufacturing Methods For Space Systems Brings Unique Properties Of Bulk Metallic Glasses (Bmg) Into The Spotlight. In Addition To Superior Mechanical Properties Associated With Enhanced Reliability, Bmg Technology Can Offer New Manufacturing Processes That Result In Components With Higher Precision And Complexity, Eliminating Machining And Minimizing Final Assembly. In This Project, We Propose To Utilize The Unique Thermoplastic Forming (Tpf) Ability Of Bmgs To Net Shape High Precision Robotic Gears. Within Phase I, We Have Proven Feasibility Of This Technology. The Technical Objectives For Phase Ii Is To Further Advance The Technology To A Level That Allows Nasa To Test And Use Bmg Gears In Nasa Missions. This Requires High Precision, Repeatability, Robustness, And Consistency Of Fabricated Parts. In Addition, A Technical Focus Will Be On Expanding The Versatility Of Tpf-Based Fabrication Process In Terms Of The Range Of Geometries And Sizes Of Flexsplines And The Range Of Bmg Alloys That Can Be Used With Tpf Processes. Identifying The Suite Of Bmg Alloys That Can Be Used For Tpf-Based Molding Would Provide Nasa With An Option To Select The Best Property Combinations In Terms Of Specific Strength, Ductility, Wear, Friction, And Costs. An Additional Technical Objective Is To Develop Strategies To Reduce Friction And Wear Through Surface Finish Of The Molded Flexsplines And Fabrication Of Surface Composites In A One Processing Step. The Outcome Of The Project Will Be Manufacturing Capabilities For Precision Robotic Components And Ready-To-Test Flexspline Gear Parts With Complex Thin Walled Geometries, Improved Properties And Dimensions Suitable For Europa Lander And Kennedy Space Center And Other Nasa S Locations. Beyond Space Applications, The Use Of Versatile Thermoplastic Forming Processes For Precision Gears Has A Strong Potential To Bring Cost Savings For A Wide Range Of Industries That Use Robotic Mechanisms.
- 25 Apr 2023
- E014042 Demand For Novel Manufacturing Methods For Space Systems Brings Unique Properties Of Bulk Metallic Glasses (Bmg) Into The Spotlight. In Addition To Superior Mechanical Properties Associated With Enhanced Reliability, Bmg Technology Can Offer New Manufacturing Processes That Result In Components With Higher Precision And Complexity, Eliminating Machining And Minimizing Final Assembly. In This Project, We Propose To Utilize The Unique Thermoplastic Forming (Tpf) Ability Of Bmgs To Net Shape High Precision Robotic Gears. Within Phase I, We Have Proven Feasibility Of This Technology. The Technical Objectives For Phase Ii Is To Further Advance The Technology To A Level That Allows Nasa To Test And Use Bmg Gears In Nasa Missions. This Requires High Precision, Repeatability, Robustness, And Consistency Of Fabricated Parts. In Addition, A Technical Focus Will Be On Expanding The Versatility Of Tpf-Based Fabrication Process In Terms Of The Range Of Geometries And Sizes Of Flexsplines And The Range Of Bmg Alloys That Can Be Used With Tpf Processes. Identifying The Suite Of Bmg Alloys That Can Be Used For Tpf-Based Molding Would Provide Nasa With An Option To Select The Best Property Combinations In Terms Of Specific Strength, Ductility, Wear, Friction, And Costs. An Additional Technical Objective Is To Develop Strategies To Reduce Friction And Wear Through Surface Finish Of The Molded Flexsplines And Fabrication Of Surface Composites In A One Processing Step. The Outcome Of The Project Will Be Manufacturing Capabilities For Precision Robotic Components And Ready-To-Test Flexspline Gear Parts With Complex Thin Walled Geometries, Improved Properties And Dimensions Suitable For Europa Lander And Kennedy Space Center And Other Nasa S Locations. Beyond Space Applications, The Use Of Versatile Thermoplastic Forming Processes For Precision Gears Has A Strong Potential To Bring Cost Savings For A Wide Range Of Industries That Use Robotic Mechanisms.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $899,131.00
- National Aeronautics And Space Administration (Nasa)