Atsp Innovations Inc
CAGE Code: 66PY6
NCAGE Code: 66PY6
Status: Active
Type: Commercial Supplier
Dun & Bradstreet (DUNS): 965433035
Summary
Atsp Innovations Inc is an Active Commercial Supplier with the Cage Code 66PY6 and is tracked by Dun & Bradstreet under DUNS Number 965433035..
Address
6762 Shadyvilla Ln Bldg 3
Houston TX 77055-5237
United States
Points of Contact
No Points of Contact...
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Frequently Asked Questions (FAQ) for CAGE 66PY6
- What is CAGE Code 66PY6?
- 66PY6 is the unique identifier used by NATO Organizations to reference the physical entity known as Atsp Innovations Inc located at 6762 Shadyvilla Ln Bldg 3, Houston TX 77055-5237, United States.
- Who is CAGE Code 66PY6?
- 66PY6 refers to Atsp Innovations Inc located at 6762 Shadyvilla Ln Bldg 3, Houston TX 77055-5237, United States.
- Where is CAGE Code 66PY6 Located?
- CAGE Code 66PY6 is located in Houston, TX, USA.
Contracting History for CAGE 66PY6 Most Recent 25 Records
- 80NSSC23PB359
- Sbir Phase I - Dust Tolerant Dynamic Seal Material For Extreme Lunar Atmosphere.
- 13 Jul 2023
- Sbir Phase I - Dust Tolerant Dynamic Seal Material For Extreme Lunar Atmosphere.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $149,911.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC23CA211
- Fy23 Phase Ii Sequential - High Performance Polymer For Dust Tolerant Extreme Environment Bearings
- 26 Sep 2023
- Fy23 Phase Ii Sequential - High Performance Polymer For Dust Tolerant Extreme Environment Bearings
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $3,211,836.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC20C0180
- E014042 Extreme Environment Tribological Characterization Of Advanced Bearing Materials
- 11 Aug 2022
- E014042 Extreme Environment Tribological Characterization Of Advanced Bearing Materials
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $754,981.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC20C0180
- Extreme Environment Tribological Characterization Of Advanced Bearing Materials
- 29 Dec 2022
- Extreme Environment Tribological Characterization Of Advanced Bearing Materials
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $754,981.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC20C0180
- Eo14042 Extreme Environment Tribological Characterization Of Advanced Bearing Materials
- 18 Oct 2021
- Eo14042 Extreme Environment Tribological Characterization Of Advanced Bearing Materials
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $754,981.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC20C0180
- Extreme Environment Tribological Characterization Of Advanced Bearing Materials
- 30 Sep 2020
- Extreme Environment Tribological Characterization Of Advanced Bearing Materials
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $754,981.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC20C0180
- Extreme Environment Tribological Characterization Of Advanced Bearing Materials
- 10 Apr 2023
- Extreme Environment Tribological Characterization Of Advanced Bearing Materials
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $904,981.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC20C0180
- Extreme Environment Tribological Characterization Of Advanced Bearing Materials
- 23 Feb 2021
- Extreme Environment Tribological Characterization Of Advanced Bearing Materials
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $754,981.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC20C0418
- Ultra-High Temperature Elastomer Sealing Materials
- 10 Feb 2021
- Ultra-High Temperature Elastomer Sealing Materials
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,669.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0134
- Surface Micro-Texturing Of Advanced Bearing Materials For Lunar Dust Mitigation
- 5 May 2021
- Surface Micro-Texturing Of Advanced Bearing Materials For Lunar Dust Mitigation
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,895.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0136
- In-Space Testing Of Reversible Adhesive System
- 15 May 2021
- In-Space Testing Of Reversible Adhesive System
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,954.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18C0040
- Atsp Innovations Will Develop A Reversible Adhesion Concept For Use In Reconfigurable Space Frame Construction. This Reversible Adhesion Concept Is Based On Application Of Aromatic Thermosetting Copolyester (Atsp) To Selected Adhesive Contact Points. By Virtue Of A Class Of Reversible Solid-State Chemical Reactions (Called Interchain Transesterification Reactions - Itr) Intrinsic To The Polymer, Atsp Was Shown To Bond And Debond With Itself For ≫50 Cycles During The Phase I With High Mechanical Strength Allowing Load Values ≫6 The Requirement Of The Solicitation In An Very Small Contact Area. In Phase Ii Of This Project We Will Apply This Reversible Adhesive Concept To Assembly And Reconfiguration Of Truss Structures Composed Of Tubular Beams And We Will Do Electrical, Thermal And Mechanical Characterizations Of The Reversibly Joined Tube Segments. Based On The Reversible Adhesion Concept Developed And Demonstrated In Phase I, A Self-Aligning Attachment Mechanism For Tubular Beams And Hub Joints With Integrated Heating Is Proposed. Designed Attachment Mechanisms And Developed Processes Will Be Applied To Assembly And Reconfiguration Of Truss Unit Cell. Polymeric Reversible Adhesive Will Be Subjected To Outgassing And Radiation Experiments (To Determine Applicability To Space Environment) In Simulation Of Low Earth Orbit With Additional Bond/Debond Cycles Following Radiation Exposure Implemented Via A Toolkit Developed In Phase I. The High Mechanical Strength Provides Design Flexibility For Space In The Joints For Electrical Contacts, Thereby Allowing Multifunctionality Of The Space Structures With Full Scale Dimension Of The Real Truss Structure, The Joint Would Be Able To Reach A Bond Strength Of 56,760N (113 Times The Required 500N).
- 3 Mar 2021
- Atsp Innovations Will Develop A Reversible Adhesion Concept For Use In Reconfigurable Space Frame Construction. This Reversible Adhesion Concept Is Based On Application Of Aromatic Thermosetting Copolyester (Atsp) To Selected Adhesive Contact Points. By Virtue Of A Class Of Reversible Solid-State Chemical Reactions (Called Interchain Transesterification Reactions - Itr) Intrinsic To The Polymer, Atsp Was Shown To Bond And Debond With Itself For ≫50 Cycles During The Phase I With High Mechanical Strength Allowing Load Values ≫6 The Requirement Of The Solicitation In An Very Small Contact Area. In Phase Ii Of This Project We Will Apply This Reversible Adhesive Concept To Assembly And Reconfiguration Of Truss Structures Composed Of Tubular Beams And We Will Do Electrical, Thermal And Mechanical Characterizations Of The Reversibly Joined Tube Segments. Based On The Reversible Adhesion Concept Developed And Demonstrated In Phase I, A Self-Aligning Attachment Mechanism For Tubular Beams And Hub Joints With Integrated Heating Is Proposed. Designed Attachment Mechanisms And Developed Processes Will Be Applied To Assembly And Reconfiguration Of Truss Unit Cell. Polymeric Reversible Adhesive Will Be Subjected To Outgassing And Radiation Experiments (To Determine Applicability To Space Environment) In Simulation Of Low Earth Orbit With Additional Bond/Debond Cycles Following Radiation Exposure Implemented Via A Toolkit Developed In Phase I. The High Mechanical Strength Provides Design Flexibility For Space In The Joints For Electrical Contacts, Thereby Allowing Multifunctionality Of The Space Structures With Full Scale Dimension Of The Real Truss Structure, The Joint Would Be Able To Reach A Bond Strength Of 56,760N (113 Times The Required 500N).
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,992.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0055
- Reversible Adhesion Concept For In-Space Assembly
- 13 Sep 2023
- Reversible Adhesion Concept For In-Space Assembly
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $187,500.00
- National Aeronautics And Space Administration (Nasa)
- 140D0420C0039
- Slender Dielectric Elastomer Fibers For Artificial Muscles
- 5 Feb 2020
- Slender Dielectric Elastomer Fibers For Artificial Muscles
- Ibc Acq Svcs Directorate (00004)
- Department Of The Interior (Doi)
- $224,777.00
- Department Of The Interior (Doi)
- 80NSSC20C0582
- Creep-Resistant Aromatic Polyester Thermosets For Thin-Ply Composites
- 25 Aug 2020
- Creep-Resistant Aromatic Polyester Thermosets For Thin-Ply Composites
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,979.00
- National Aeronautics And Space Administration (Nasa)
- FA945323PA039
- Reversible Thermally Driven Adhesive (Rtda) For On-Orbit Assembly
- 16 Mar 2023
- Reversible Thermally Driven Adhesive (Rtda) For On-Orbit Assembly
- Fa9453 Afrl Rvk
- Department Of Defense (Dod)
- $149,999.00
- Department Of Defense (Dod)
- 140D0420C0039
- Slender Dielectric Elastomer Fibers For Artificial Muscles
- 30 Jul 2020
- Slender Dielectric Elastomer Fibers For Artificial Muscles
- Ibc Acq Svcs Directorate (00004)
- Department Of The Interior (Doi)
- $224,777.00
- Department Of The Interior (Doi)
- 80NSSC18C0040
- Atsp Innovations Will Develop A Reversible Adhesion Concept For Use In Reconfigurable Space Frame Construction. This Reversible Adhesion Concept Is Based On Application Of Aromatic Thermosetting Copolyester (Atsp) To Selected Adhesive Contact Points. By Virtue Of A Class Of Reversible Solid-State Chemical Reactions (Called Interchain Transesterification Reactions - Itr) Intrinsic To The Polymer, Atsp Was Shown To Bond And Debond With Itself For≫50 Cycles During The Phase I With High Mechanical Strength Allowing Load Values≫6 The Requirement Of The Solicitation In An Very Small Contact Area. In Phase Ii Of This Project We Will Apply This Reversible Adhesive Concept To Assembly And Reconfiguration Of Truss Structures Composed Of Tubular Beams And We Will Do Electrical, Thermal And Mechanical Characterizations Of The Reversibly Joined Tube Segments. Based On The Reversible Adhesion Concept Developed And Demonstrated In Phase I, A Self-Aligning Attachment Mechanism For Tubular Beams And Hub Joints With Integrated Heating Is Proposed. Designed Attachment Mechanisms And Developed Processes Will Be Applied To Assembly And Reconfiguration Of Truss Unit Cell. Polymeric Reversible Adhesive Will Be Subjected To Outgassing And Radiation Experiments (To Determine Applicability To Space Environment) In Simulation Of Low Earth Orbit With Additional Bond/Debond Cycles Following Radiation Exposure Implemented Via A Toolkit Developed In Phase I. The High Mechanical Strength Provides Design Flexibility For Space In The Joints For Electrical Contacts, Thereby Allowing Multifunctionality Of The Space Structures With Full Scale Dimension Of The Real Truss Structure, The Joint Would Be Able To Reach A Bond Strength Of 56,760N (113 Times The Required 500N).
- 25 Mar 2020
- Atsp Innovations Will Develop A Reversible Adhesion Concept For Use In Reconfigurable Space Frame Construction. This Reversible Adhesion Concept Is Based On Application Of Aromatic Thermosetting Copolyester (Atsp) To Selected Adhesive Contact Points. By Virtue Of A Class Of Reversible Solid-State Chemical Reactions (Called Interchain Transesterification Reactions - Itr) Intrinsic To The Polymer, Atsp Was Shown To Bond And Debond With Itself For≫50 Cycles During The Phase I With High Mechanical Strength Allowing Load Values≫6 The Requirement Of The Solicitation In An Very Small Contact Area. In Phase Ii Of This Project We Will Apply This Reversible Adhesive Concept To Assembly And Reconfiguration Of Truss Structures Composed Of Tubular Beams And We Will Do Electrical, Thermal And Mechanical Characterizations Of The Reversibly Joined Tube Segments. Based On The Reversible Adhesion Concept Developed And Demonstrated In Phase I, A Self-Aligning Attachment Mechanism For Tubular Beams And Hub Joints With Integrated Heating Is Proposed. Designed Attachment Mechanisms And Developed Processes Will Be Applied To Assembly And Reconfiguration Of Truss Unit Cell. Polymeric Reversible Adhesive Will Be Subjected To Outgassing And Radiation Experiments (To Determine Applicability To Space Environment) In Simulation Of Low Earth Orbit With Additional Bond/Debond Cycles Following Radiation Exposure Implemented Via A Toolkit Developed In Phase I. The High Mechanical Strength Provides Design Flexibility For Space In The Joints For Electrical Contacts, Thereby Allowing Multifunctionality Of The Space Structures With Full Scale Dimension Of The Real Truss Structure, The Joint Would Be Able To Reach A Bond Strength Of 56,760N (113 Times The Required 500N).
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,992.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0055
- Reversible Adhesion Concept For In-Space Assembly
- 29 Jun 2021
- Reversible Adhesion Concept For In-Space Assembly
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $0.01
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0055
- E014042 Reversible Adhesion Concept For In-Space Assembly
- 5 May 2023
- E014042 Reversible Adhesion Concept For In-Space Assembly
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $187,500.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0055
- Reversible Adhesion Concept For In-Space Assembly
- 11 May 2021
- Reversible Adhesion Concept For In-Space Assembly
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $187,500.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0056
- Eo14042 Reversible Adhesion Concept For In-Space Assembly
- 16 Nov 2022
- Eo14042 Reversible Adhesion Concept For In-Space Assembly
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $187,500.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0055
- Reversible Adhesion Concept For In-Space Assembly
- 30 Jun 2021
- Reversible Adhesion Concept For In-Space Assembly
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $187,500.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18C0040
- Atsp Innovations Will Develop A Reversible Adhesion Concept For Use In Reconfigurable Space Frame Construction. This Reversible Adhesion Concept Is Based On Application Of Aromatic Thermosetting Copolyester (Atsp) To Selected Adhesive Contact Points. By Virtue Of A Class Of Reversible Solid-State Chemical Reactions (Called Interchain Transesterification Reactions - Itr) Intrinsic To The Polymer, Atsp Was Shown To Bond And Debond With Itself For>50 Cycles During The Phase I With High Mechanical Strength Allowing Load Values>6 The Requirement Of The Solicitation In An Very Small Contact Area. In Phase Ii Of This Project We Will Apply This Reversible Adhesive Concept To Assembly And Reconfiguration Of Truss Structures Composed Of Tubular Beams And We Will Do Electrical, Thermal And Mechanical Characterizations Of The Reversibly Joined Tube Segments. Based On The Reversible Adhesion Concept Developed And Demonstrated In Phase I, A Self-Aligning Attachment Mechanism For Tubular Beams And Hub Joints With Integrated Heating Is Proposed. Designed Attachment Mechanisms And Developed Processes Will Be Applied To Assembly And Reconfiguration Of Truss Unit Cell. Polymeric Reversible Adhesive Will Be Subjected To Outgassing And Radiation Experiments (To Determine Applicability To Space Environment) In Simulation Of Low Earth Orbit With Additional Bond/Debond Cycles Following Radiation Exposure Implemented Via A Toolkit Developed In Phase I. The High Mechanical Strength Provides Design Flexibility For Space In The Joints For Electrical Contacts, Thereby Allowing Multifunctionality Of The Space Structures; With Full Scale Dimension Of The Real Truss Structure, The Joint Would Be Able To Reach A Bond Strength Of 56,760N (113 Times The Required 500N).
- 18 May 2018
- Atsp Innovations Will Develop A Reversible Adhesion Concept For Use In Reconfigurable Space Frame Construction. This Reversible Adhesion Concept Is Based On Application Of Aromatic Thermosetting Copolyester (Atsp) To Selected Adhesive Contact Points. By Virtue Of A Class Of Reversible Solid-State Chemical Reactions (Called Interchain Transesterification Reactions - Itr) Intrinsic To The Polymer, Atsp Was Shown To Bond And Debond With Itself For>50 Cycles During The Phase I With High Mechanical Strength Allowing Load Values>6 The Requirement Of The Solicitation In An Very Small Contact Area. In Phase Ii Of This Project We Will Apply This Reversible Adhesive Concept To Assembly And Reconfiguration Of Truss Structures Composed Of Tubular Beams And We Will Do Electrical, Thermal And Mechanical Characterizations Of The Reversibly Joined Tube Segments. Based On The Reversible Adhesion Concept Developed And Demonstrated In Phase I, A Self-Aligning Attachment Mechanism For Tubular Beams And Hub Joints With Integrated Heating Is Proposed. Designed Attachment Mechanisms And Developed Processes Will Be Applied To Assembly And Reconfiguration Of Truss Unit Cell. Polymeric Reversible Adhesive Will Be Subjected To Outgassing And Radiation Experiments (To Determine Applicability To Space Environment) In Simulation Of Low Earth Orbit With Additional Bond/Debond Cycles Following Radiation Exposure Implemented Via A Toolkit Developed In Phase I. The High Mechanical Strength Provides Design Flexibility For Space In The Joints For Electrical Contacts, Thereby Allowing Multifunctionality Of The Space Structures; With Full Scale Dimension Of The Real Truss Structure, The Joint Would Be Able To Reach A Bond Strength Of 56,760N (113 Times The Required 500N).
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,992.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC20C0418
- Ultra-High Temperature Elastomer Sealing Materials
- 24 Aug 2020
- Ultra-High Temperature Elastomer Sealing Materials
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,669.00
- National Aeronautics And Space Administration (Nasa)