Kaneka Aerospace Llc
CAGE Code: 1JMQ1
NCAGE Code: 1JMQ1
Status: Active
Type: Manufacturer
Dun & Bradstreet (DUNS): 787223460
Summary
Kaneka Aerospace Llc is an Active Manufacturer with the Cage Code 1JMQ1 and is tracked by Dun & Bradstreet under DUNS Number 787223460..
Address
6166 Egret Ct
Benicia CA 94510-1269
United States
Points of Contact
No Points of Contact...
Related Information
People who viewed this 'CAGE Code' also viewed...
S & S Investment Club Bw/Ip Intl Inc Century Safety Global Marketing And Sales Specialty Products And Insulation Philip Korbas Human Behavior Associates Inc Tejas Energy Environmental Service Oon Site Tageson Maritime Consulting Abm Building Solutions Llc Underground Construction Company, Terry F Schillinger, Ii Browning-Ferris Industries Inc Environmental Contracting-Pacific Goodyear Commercial Tire And Service Gcxinc. Tlc Transportation Larson-Juhl A And J Glass
Frequently Asked Questions (FAQ) for CAGE 1JMQ1
- What is CAGE Code 1JMQ1?
- 1JMQ1 is the unique identifier used by NATO Organizations to reference the physical entity known as Kaneka Aerospace Llc located at 6166 Egret Ct, Benicia CA 94510-1269, United States.
- Who is CAGE Code 1JMQ1?
- 1JMQ1 refers to Kaneka Aerospace Llc located at 6166 Egret Ct, Benicia CA 94510-1269, United States.
- Where is CAGE Code 1JMQ1 Located?
- CAGE Code 1JMQ1 is located in Benicia, CA, USA.
Contracting History for CAGE 1JMQ1 Most Recent 25 Records
- NNX16CM12C
- Igf::Ot::Igf As The Size Of Composite Parts Exceed That Of Even The Largest Autoclaves, New Out-Of-Autoclave Processes And Materials Are Necessary To Achieve The Same Level Of Performance As Autoclave Cured Composites. As An Alternative To Ooa Prepreg Systems, Infusion Of Dry Fiber Preforms Made By Automated Dry Fiber Placement (Adfp) Can Mitigate Out-Time Issues And Shelf-Life Problems Combined With Lower Cost Manufacturing. Although Improvements In Adfp Products Have Continued, Use And Application Of These Adfp Products Have Been Limited Due To The Necessary Balance Of Processing And Performance Of The Infusion Resin. This Is A Result Of Not Only The Low Permeability Of The Adfp Product Preforms But Also The Inadequate Damage Tolerance And Micro-Crack Sensitivity Of The Developed Composites. Accordingly, Applied Poleramic, Inc. Proposes To Develop A Novel Low Viscosity, Long Pot-Life Infusion Resin For Use With Adfp Product Preforms That Results In Cured Performance Similar To That Of Unidirectional Hexcel 8552 Prepreg Parts. Specifically, The Infusion Resin Will Be Capable Of Significantly Lower Infusion Temperature (Less Than 150 F) As Compared To Current Commercial Infusion Resins Along With Improved Fracture Toughness. This Innovative Epoxy Infusion Resin Will Enable Large Complex Composite Structures To Be Developed Using Adfp Product Preforms With Lower Manufacturing Risk, Reduced Production Time, Higher Part Quality, And A New Level Of Performance Not Attainable With Current Commercial Infusion Resins. Ultimately, The Technology Will Lead To A New Generation Of Low Cost Composite Materials, Critical To Future Nasa Space Programs And Missions.
- 5 Jun 2018
- Igf::Ot::Igf As The Size Of Composite Parts Exceed That Of Even The Largest Autoclaves, New Out-Of-Autoclave Processes And Materials Are Necessary To Achieve The Same Level Of Performance As Autoclave Cured Composites. As An Alternative To Ooa Prepreg Systems, Infusion Of Dry Fiber Preforms Made By Automated Dry Fiber Placement (Adfp) Can Mitigate Out-Time Issues And Shelf-Life Problems Combined With Lower Cost Manufacturing. Although Improvements In Adfp Products Have Continued, Use And Application Of These Adfp Products Have Been Limited Due To The Necessary Balance Of Processing And Performance Of The Infusion Resin. This Is A Result Of Not Only The Low Permeability Of The Adfp Product Preforms But Also The Inadequate Damage Tolerance And Micro-Crack Sensitivity Of The Developed Composites. Accordingly, Applied Poleramic, Inc. Proposes To Develop A Novel Low Viscosity, Long Pot-Life Infusion Resin For Use With Adfp Product Preforms That Results In Cured Performance Similar To That Of Unidirectional Hexcel 8552 Prepreg Parts. Specifically, The Infusion Resin Will Be Capable Of Significantly Lower Infusion Temperature (Less Than 150 F) As Compared To Current Commercial Infusion Resins Along With Improved Fracture Toughness. This Innovative Epoxy Infusion Resin Will Enable Large Complex Composite Structures To Be Developed Using Adfp Product Preforms With Lower Manufacturing Risk, Reduced Production Time, Higher Part Quality, And A New Level Of Performance Not Attainable With Current Commercial Infusion Resins. Ultimately, The Technology Will Lead To A New Generation Of Low Cost Composite Materials, Critical To Future Nasa Space Programs And Missions.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $745,850.00
- National Aeronautics And Space Administration (Nasa)
- FA865015C5079
- Igf::Ot::Igf Standard Test Method For Prepreg Resin Impregnation Level
- 11 May 2018
- Igf::Ot::Igf Standard Test Method For Prepreg Resin Impregnation Level
- Dcma Stockton
- Department Of Defense (Dod)
- $741,325.00
- Department Of Defense (Dod)
- N6833513C0278
- Research&Development
- 11 May 2018
- Research&Development
- Dcma Stockton
- Department Of Defense (Dod)
- $748,610.00
- Department Of Defense (Dod)
- NNX16CL14C
- Igf::Ot::Igf Radiation Shielding Materials Are Necessary For Protecting Astronaut Crews From The Hazards Of Space Radiation During Future Nasa Missions. Although Polyethylene Based Materials And Composites Are Attractive For Radiation Shielding Due To High Hydrogen Content, The Poor Thermal Performance Has Limited Its Use As A Parasitic, Nonstructural Material. Further Impeding Use Of This Material Is Its Inherent Flammability. Accordingly, Thermally Stable Structural Materials Having Low Flammability Combined With Radiation Shielding Are Necessary For The Development Of Next Generation Aerospace Structures And Vehicles. It Would Be Further Desirable That The Non-Parasitic Material Has Excellent Damage Tolerance To Mitigate Impact Events In Operation. Applied Poleramic, Inc. Proposes To Develop A New Generation Of Structural High Hydrogen Content Matrix Materials Which Will Be Combined With An Interlayer Modification Approach To Result In Fiber Reinforced Composite Materials Having Enhanced Radiation Shielding Combined With Excellent Damage Tolerance And Improved Flammability Resistance.
- 6 Jun 2018
- Igf::Ot::Igf Radiation Shielding Materials Are Necessary For Protecting Astronaut Crews From The Hazards Of Space Radiation During Future Nasa Missions. Although Polyethylene Based Materials And Composites Are Attractive For Radiation Shielding Due To High Hydrogen Content, The Poor Thermal Performance Has Limited Its Use As A Parasitic, Nonstructural Material. Further Impeding Use Of This Material Is Its Inherent Flammability. Accordingly, Thermally Stable Structural Materials Having Low Flammability Combined With Radiation Shielding Are Necessary For The Development Of Next Generation Aerospace Structures And Vehicles. It Would Be Further Desirable That The Non-Parasitic Material Has Excellent Damage Tolerance To Mitigate Impact Events In Operation. Applied Poleramic, Inc. Proposes To Develop A New Generation Of Structural High Hydrogen Content Matrix Materials Which Will Be Combined With An Interlayer Modification Approach To Result In Fiber Reinforced Composite Materials Having Enhanced Radiation Shielding Combined With Excellent Damage Tolerance And Improved Flammability Resistance.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $740,036.00
- National Aeronautics And Space Administration (Nasa)
- NNX16CM12C
- Igf::Ot::Igf As The Size Of Composite Parts Exceed That Of Even The Largest Autoclaves, New Out-Of-Autoclave Processes And Materials Are Necessary To Achieve The Same Level Of Performance As Autoclave Cured Composites. As An Alternative To Ooa Prepreg Systems, Infusion Of Dry Fiber Preforms Made By Automated Dry Fiber Placement (Adfp) Can Mitigate Out-Time Issues And Shelf-Life Problems Combined With Lower Cost Manufacturing. Although Improvements In Adfp Products Have Continued, Use And Application Of These Adfp Products Have Been Limited Due To The Necessary Balance Of Processing And Performance Of The Infusion Resin. This Is A Result Of Not Only The Low Permeability Of The Adfp Product Preforms But Also The Inadequate Damage Tolerance And Micro-Crack Sensitivity Of The Developed Composites. Accordingly, Applied Poleramic, Inc. Proposes To Develop A Novel Low Viscosity, Long Pot-Life Infusion Resin For Use With Adfp Product Preforms That Results In Cured Performance Similar To That Of Unidirectional Hexcel 8552 Prepreg Parts. Specifically, The Infusion Resin Will Be Capable Of Significantly Lower Infusion Temperature (Less Than 150 F) As Compared To Current Commercial Infusion Resins Along With Improved Fracture Toughness. This Innovative Epoxy Infusion Resin Will Enable Large Complex Composite Structures To Be Developed Using Adfp Product Preforms With Lower Manufacturing Risk, Reduced Production Time, Higher Part Quality, And A New Level Of Performance Not Attainable With Current Commercial Infusion Resins. Ultimately, The Technology Will Lead To A New Generation Of Low Cost Composite Materials, Critical To Future Nasa Space Programs And Missions.
- 4 Jun 2018
- Igf::Ot::Igf As The Size Of Composite Parts Exceed That Of Even The Largest Autoclaves, New Out-Of-Autoclave Processes And Materials Are Necessary To Achieve The Same Level Of Performance As Autoclave Cured Composites. As An Alternative To Ooa Prepreg Systems, Infusion Of Dry Fiber Preforms Made By Automated Dry Fiber Placement (Adfp) Can Mitigate Out-Time Issues And Shelf-Life Problems Combined With Lower Cost Manufacturing. Although Improvements In Adfp Products Have Continued, Use And Application Of These Adfp Products Have Been Limited Due To The Necessary Balance Of Processing And Performance Of The Infusion Resin. This Is A Result Of Not Only The Low Permeability Of The Adfp Product Preforms But Also The Inadequate Damage Tolerance And Micro-Crack Sensitivity Of The Developed Composites. Accordingly, Applied Poleramic, Inc. Proposes To Develop A Novel Low Viscosity, Long Pot-Life Infusion Resin For Use With Adfp Product Preforms That Results In Cured Performance Similar To That Of Unidirectional Hexcel 8552 Prepreg Parts. Specifically, The Infusion Resin Will Be Capable Of Significantly Lower Infusion Temperature (Less Than 150 F) As Compared To Current Commercial Infusion Resins Along With Improved Fracture Toughness. This Innovative Epoxy Infusion Resin Will Enable Large Complex Composite Structures To Be Developed Using Adfp Product Preforms With Lower Manufacturing Risk, Reduced Production Time, Higher Part Quality, And A New Level Of Performance Not Attainable With Current Commercial Infusion Resins. Ultimately, The Technology Will Lead To A New Generation Of Low Cost Composite Materials, Critical To Future Nasa Space Programs And Missions.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $745,850.00
- National Aeronautics And Space Administration (Nasa)
- NNX16CL14C
- Igf::Ot::Igf Radiation Shielding Materials Are Necessary For Protecting Astronaut Crews From The Hazards Of Space Radiation During Future Nasa Missions. Although Polyethylene Based Materials And Composites Are Attractive For Radiation Shielding Due To High Hydrogen Content, The Poor Thermal Performance Has Limited Its Use As A Parasitic, Nonstructural Material. Further Impeding Use Of This Material Is Its Inherent Flammability. Accordingly, Thermally Stable Structural Materials Having Low Flammability Combined With Radiation Shielding Are Necessary For The Development Of Next Generation Aerospace Structures And Vehicles. It Would Be Further Desirable That The Non-Parasitic Material Has Excellent Damage Tolerance To Mitigate Impact Events In Operation. Applied Poleramic, Inc. Proposes To Develop A New Generation Of Structural High Hydrogen Content Matrix Materials Which Will Be Combined With An Interlayer Modification Approach To Result In Fiber Reinforced Composite Materials Having Enhanced Radiation Shielding Combined With Excellent Damage Tolerance And Improved Flammability Resistance.
- 13 Nov 2018
- Igf::Ot::Igf Radiation Shielding Materials Are Necessary For Protecting Astronaut Crews From The Hazards Of Space Radiation During Future Nasa Missions. Although Polyethylene Based Materials And Composites Are Attractive For Radiation Shielding Due To High Hydrogen Content, The Poor Thermal Performance Has Limited Its Use As A Parasitic, Nonstructural Material. Further Impeding Use Of This Material Is Its Inherent Flammability. Accordingly, Thermally Stable Structural Materials Having Low Flammability Combined With Radiation Shielding Are Necessary For The Development Of Next Generation Aerospace Structures And Vehicles. It Would Be Further Desirable That The Non-Parasitic Material Has Excellent Damage Tolerance To Mitigate Impact Events In Operation. Applied Poleramic, Inc. Proposes To Develop A New Generation Of Structural High Hydrogen Content Matrix Materials Which Will Be Combined With An Interlayer Modification Approach To Result In Fiber Reinforced Composite Materials Having Enhanced Radiation Shielding Combined With Excellent Damage Tolerance And Improved Flammability Resistance.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $740,036.00
- National Aeronautics And Space Administration (Nasa)
- NNX16CL14C
- Igf::Ot::Igf Radiation Shielding Materials Are Necessary For Protecting Astronaut Crews From The Hazards Of Space Radiation During Future Nasa Missions. Although Polyethylene Based Materials And Composites Are Attractive For Radiation Shielding Due To High Hydrogen Content, The Poor Thermal Performance Has Limited Its Use As A Parasitic, Nonstructural Material. Further Impeding Use Of This Material Is Its Inherent Flammability. Accordingly, Thermally Stable Structural Materials Having Low Flammability Combined With Radiation Shielding Are Necessary For The Development Of Next Generation Aerospace Structures And Vehicles. It Would Be Further Desirable That The Non-Parasitic Material Has Excellent Damage Tolerance To Mitigate Impact Events In Operation. Applied Poleramic, Inc. Proposes To Develop A New Generation Of Structural High Hydrogen Content Matrix Materials Which Will Be Combined With An Interlayer Modification Approach To Result In Fiber Reinforced Composite Materials Having Enhanced Radiation Shielding Combined With Excellent Damage Tolerance And Improved Flammability Resistance.
- 6 Jun 2018
- Igf::Ot::Igf Radiation Shielding Materials Are Necessary For Protecting Astronaut Crews From The Hazards Of Space Radiation During Future Nasa Missions. Although Polyethylene Based Materials And Composites Are Attractive For Radiation Shielding Due To High Hydrogen Content, The Poor Thermal Performance Has Limited Its Use As A Parasitic, Nonstructural Material. Further Impeding Use Of This Material Is Its Inherent Flammability. Accordingly, Thermally Stable Structural Materials Having Low Flammability Combined With Radiation Shielding Are Necessary For The Development Of Next Generation Aerospace Structures And Vehicles. It Would Be Further Desirable That The Non-Parasitic Material Has Excellent Damage Tolerance To Mitigate Impact Events In Operation. Applied Poleramic, Inc. Proposes To Develop A New Generation Of Structural High Hydrogen Content Matrix Materials Which Will Be Combined With An Interlayer Modification Approach To Result In Fiber Reinforced Composite Materials Having Enhanced Radiation Shielding Combined With Excellent Damage Tolerance And Improved Flammability Resistance.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $740,036.00
- National Aeronautics And Space Administration (Nasa)