Angstrom Designs Inc
Dba Angstrom Designs
CAGE Code: 4QE10
NCAGE Code: 4QE10
Status: Active
Type: Manufacturer
Dun & Bradstreet (DUNS): 796519630
Summary
Angstrom Designs Inc, Dba Angstrom Designs is an Active Manufacturer with the Cage Code 4QE10 and is tracked by Dun & Bradstreet under DUNS Number 796519630..
Address
32 E Haley St
Santa Barbara CA 93101-2316
United States
Points of Contact
No Points of Contact...
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Frequently Asked Questions (FAQ) for CAGE 4QE10
- What is CAGE Code 4QE10?
- 4QE10 is the unique identifier used by NATO Organizations to reference the physical entity known as Angstrom Designs Inc Dba Angstrom Designs located at 32 E Haley St, Santa Barbara CA 93101-2316, United States.
- Who is CAGE Code 4QE10?
- 4QE10 refers to Angstrom Designs Inc Dba Angstrom Designs located at 32 E Haley St, Santa Barbara CA 93101-2316, United States.
- Where is CAGE Code 4QE10 Located?
- CAGE Code 4QE10 is located in Santa Barbara, CA, USA.
Contracting History for CAGE 4QE10 Most Recent 25 Records
- FA945322CA105
- 6 Junction Expansion To 3-5 Junction Programmable Led Solar Simulator
- 9 Sep 2022
- 6 Junction Expansion To 3-5 Junction Programmable Led Solar Simulator
- Fa9453 Afrl Rvk
- Department Of Defense (Dod)
- $749,657.75
- Department Of Defense (Dod)
- FA881418C0003
- Restoring National Solar Cell Calibration Balloon Flight Capability Rapid Innovation Fund Aware To Angstrom
- 29 Jul 2021
- Restoring National Solar Cell Calibration Balloon Flight Capability Rapid Innovation Fund Aware To Angstrom
- Fa8814 Space Dev Test Plan Pkt La
- Department Of Defense (Dod)
- $685,974.00
- Department Of Defense (Dod)
- FA881418C0003
- Restoring National Solar Cell Calibration Balloon Flight Capability Rapid Innovation Fund Award To Angstrom.
- 15 Mar 2022
- Restoring National Solar Cell Calibration Balloon Flight Capability Rapid Innovation Fund Award To Angstrom.
- Fa8814 Space Dev Test Plan Pkt La
- Department Of Defense (Dod)
- $960,681.00
- Department Of Defense (Dod)
- FA881418C0003
- Space Solar Cell Balloon Flight Calibration System
- 22 Aug 2023
- Space Solar Cell Balloon Flight Calibration System
- Fa8819 Special Programs Dir Smc Sp
- Department Of Defense (Dod)
- $960,681.00
- Department Of Defense (Dod)
- FA881418C0003
- Restoring National Solar Cell Calibration Balloon Flight Capability Rapid Innovation Fund Aware To Angstrom
- 26 Jan 2021
- Restoring National Solar Cell Calibration Balloon Flight Capability Rapid Innovation Fund Aware To Angstrom
- Fa8814 Space Dev Test Plan Pkt La
- Department Of Defense (Dod)
- $685,974.00
- Department Of Defense (Dod)
- FA881418C0003
- Dodaac Fa8814 To Fa8819 Space Solar Cell Balloon Flight Calibration System
- 13 Apr 2023
- Dodaac Fa8814 To Fa8819 Space Solar Cell Balloon Flight Calibration System
- Fa8819 Special Programs Dir Smc Sp
- Department Of Defense (Dod)
- $960,681.00
- Department Of Defense (Dod)
- FA881418C0003
- Restoring National Solar Cell Calibration Balloon Flight Cabability Rapid Innovation Fund Aware To Angstrom
- 4 Jun 2019
- Restoring National Solar Cell Calibration Balloon Flight Cabability Rapid Innovation Fund Aware To Angstrom
- Fa8814 Hq Smc Adk Xrk/Pkr/Adk
- Department Of Defense (Dod)
- $685,974.00
- Department Of Defense (Dod)
- 80NSSC20P0970
- Light Modules And High Voltage Controller For Our Angstrom Designs Pulsed Programmable Led Solar Simulator
- 25 Jun 2020
- Light Modules And High Voltage Controller For Our Angstrom Designs Pulsed Programmable Led Solar Simulator
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $0.00
- National Aeronautics And Space Administration (Nasa)
- FA945317C0416
- No Cost Extension (Advanced Solar Array For Dual Launch Gps)
- 14 Feb 2022
- No Cost Extension (Advanced Solar Array For Dual Launch Gps)
- Fa9453 Afrl Rvk
- Department Of Defense (Dod)
- $1,470,750.00
- Department Of Defense (Dod)
- FA881419C0009
- Period Of Performance, Revision To Attachment 1 Statement Of Work And Exhibit A Contract Data Requirements List And Update Space And Missile Center - G001 Payment Instruction July 2019.
- 6 Jul 2021
- Period Of Performance, Revision To Attachment 1 Statement Of Work And Exhibit A Contract Data Requirements List And Update Space And Missile Center - G001 Payment Instruction July 2019.
- Fa8814 Space Dev Test Plan Pkt La
- Department Of Defense (Dod)
- $1,999,121.00
- Department Of Defense (Dod)
- FA945321P0514
- Hyperspectral Microwave Imaging Radiometer
- 21 Jul 2021
- Hyperspectral Microwave Imaging Radiometer
- Fa9453 Afrl Rvk
- Department Of Defense (Dod)
- $149,701.00
- Department Of Defense (Dod)
- 80NSSC17C0020
- No Existing Commercial Wireless Sensor Network Option Meets Nasas Current Needs For Flexibility, Size, Mass And Resilience To Extreme Environments. The Proposed Innovation Is A Meis Network Which Combines Any Number And Any Type Of Sensors Into A Wireless Sensor Network (Wsn), With Each Of The Sensors Being Motes, Or Nodes, On The Network. The Network Will Be Self-Healing And Self-Configuring. Each Mote Will Consist Of Three Parts: A Communication Module, A Sensor Module, And A Power Module, And Be Fit For Rugged Applications, Ncluding For Spaceflight Hardware. There Will Also Be A Gateway, Which Acts As An Interface To The Outside World. At The Minimum, A Meis Network Requires One Sensor Node And One Gateway. As A Result Of Significant Technical Effort, The Phase I Was Successful In Delivering A Prototype Proving The Modular Embedded Wireless Sensor (Meis) Network Concept. This Also Reduces Our Risk In Proceeding Forward With Our Design. The Prototype Includes Hardware And Software, Both Custom Designed By Angstrom Designs.
- 4 Jun 2018
- No Existing Commercial Wireless Sensor Network Option Meets Nasas Current Needs For Flexibility, Size, Mass And Resilience To Extreme Environments. The Proposed Innovation Is A Meis Network Which Combines Any Number And Any Type Of Sensors Into A Wireless Sensor Network (Wsn), With Each Of The Sensors Being Motes, Or Nodes, On The Network. The Network Will Be Self-Healing And Self-Configuring. Each Mote Will Consist Of Three Parts: A Communication Module, A Sensor Module, And A Power Module, And Be Fit For Rugged Applications, Ncluding For Spaceflight Hardware. There Will Also Be A Gateway, Which Acts As An Interface To The Outside World. At The Minimum, A Meis Network Requires One Sensor Node And One Gateway. As A Result Of Significant Technical Effort, The Phase I Was Successful In Delivering A Prototype Proving The Modular Embedded Wireless Sensor (Meis) Network Concept. This Also Reduces Our Risk In Proceeding Forward With Our Design. The Prototype Includes Hardware And Software, Both Custom Designed By Angstrom Designs.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $748,816.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC20P0970
- Light Modules And High Voltage Controller For Our Angstrom Designs Pulsed Programmable Led Solar Simulator
- 29 Jul 2020
- Light Modules And High Voltage Controller For Our Angstrom Designs Pulsed Programmable Led Solar Simulator
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $197,000.00
- National Aeronautics And Space Administration (Nasa)
- FA945317C0416
- Advanced Solar Array For Dual Launch Gps
- 20 Nov 2018
- Advanced Solar Array For Dual Launch Gps
- Fa9453 Det 8 Afrl Pkv8
- Department Of Defense (Dod)
- $720,961.00
- Department Of Defense (Dod)
- FA945317C0416
- Advanced Solar Array For Dual Launch Gps
- 28 Dec 2022
- Advanced Solar Array For Dual Launch Gps
- Fa9453 Afrl Rvk
- Department Of Defense (Dod)
- $1,470,750.00
- Department Of Defense (Dod)
- FA881419C0009
- Large Area Long Pulse, Light Emitting Diode Based, Solar Simulator For 3J-6J Solar Cells
- 3 Mar 2020
- Large Area Long Pulse, Light Emitting Diode Based, Solar Simulator For 3J-6J Solar Cells
- Fa8814 Space Dev Test Plan Pkt La
- Department Of Defense (Dod)
- $1,999,121.00
- Department Of Defense (Dod)
- 80NSSC20P0970
- Light Modules And High Voltage Controller For Our Angstrom Designs Pulsed Programmable Led Solar Simulator
- 18 Nov 2020
- Light Modules And High Voltage Controller For Our Angstrom Designs Pulsed Programmable Led Solar Simulator
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $197,000.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC17C0020
- No Existing Commercial Wireless Sensor Network Option Meets Nasas Current Needs For Flexibility, Size, Mass And Resilience To Extreme Environments. The Proposed Innovation Is A Meis Network Which Combines Any Number And Any Type Of Sensors Into A Wireless Sensor Network (Wsn), With Each Of The Sensors Being Motes, Or Nodes, On The Network. The Network Will Be Self-Healing And Self-Configuring. Each Mote Will Consist Of Three Parts: A Communication Module, A Sensor Module, And A Power Module, And Be Fit For Rugged Applications, Ncluding For Spaceflight Hardware. There Will Also Be A Gateway, Which Acts As An Interface To The Outside World. At The Minimum, A Meis Network Requires One Sensor Node And One Gateway. As A Result Of Significant Technical Effort, The Phase I Was Successful In Delivering A Prototype Proving The Modular Embedded Wireless Sensor (Meis) Network Concept. This Also Reduces Our Risk In Proceeding Forward With Our Design. The Prototype Includes Hardware And Software, Both Custom Designed By Angstrom Designs.
- 24 Apr 2019
- No Existing Commercial Wireless Sensor Network Option Meets Nasas Current Needs For Flexibility, Size, Mass And Resilience To Extreme Environments. The Proposed Innovation Is A Meis Network Which Combines Any Number And Any Type Of Sensors Into A Wireless Sensor Network (Wsn), With Each Of The Sensors Being Motes, Or Nodes, On The Network. The Network Will Be Self-Healing And Self-Configuring. Each Mote Will Consist Of Three Parts: A Communication Module, A Sensor Module, And A Power Module, And Be Fit For Rugged Applications, Ncluding For Spaceflight Hardware. There Will Also Be A Gateway, Which Acts As An Interface To The Outside World. At The Minimum, A Meis Network Requires One Sensor Node And One Gateway. As A Result Of Significant Technical Effort, The Phase I Was Successful In Delivering A Prototype Proving The Modular Embedded Wireless Sensor (Meis) Network Concept. This Also Reduces Our Risk In Proceeding Forward With Our Design. The Prototype Includes Hardware And Software, Both Custom Designed By Angstrom Designs.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $748,816.00
- National Aeronautics And Space Administration (Nasa)
- FA881418C0003
- Igf::Ot::Igf Restoring National Solar Cell Calibration Balloon Flight Cabability Rapid Innovation Fund Aware To Angstrom
- 25 Jul 2018
- Igf::Ot::Igf Restoring National Solar Cell Calibration Balloon Flight Cabability Rapid Innovation Fund Aware To Angstrom
- Fa8814 Hq Smc Xr Pkr
- Department Of Defense (Dod)
- $685,974.00
- Department Of Defense (Dod)
- FA881418C0003
- Igf::Ot::Igf Angstrom Rapid Innovation Fund Line Update
- 27 Sep 2018
- Igf::Ot::Igf Angstrom Rapid Innovation Fund Line Update
- Fa8814 Hq Smc Xr Pkr
- Department Of Defense (Dod)
- $685,974.00
- Department Of Defense (Dod)
- FA881419C0009
- Rapid Innovation Fund Program
- 14 Oct 2022
- Rapid Innovation Fund Program
- Fa8814 Space Dev Test Plan Pkt La
- Department Of Defense (Dod)
- $1,999,121.00
- Department Of Defense (Dod)
- FA945317C0416
- Advanced Solar Array For Dual Launch Gps
- 14 Jun 2019
- Advanced Solar Array For Dual Launch Gps
- Fa9453 Det 8 Afrl Pkv8
- Department Of Defense (Dod)
- $720,961.00
- Department Of Defense (Dod)
- FA945317C0416
- Advanced Solar Array For Dual Launch Gps
- 4 Feb 2020
- Advanced Solar Array For Dual Launch Gps
- Fa9453 Det 8 Afrl Pkv8
- Department Of Defense (Dod)
- $1,470,750.00
- Department Of Defense (Dod)
- NNX16CL25C
- Igf::Ot::Igf Solar Arrays Power The Vast Majority Of Space Missions. Solar Arrays With Higher Power, Better Mass Efficiency And Improved Packaging Are Critical, Especially Given Nasa Interest In Solar Electric Propulsion (Sep). The Phase I Results Shows That The Compact Telescoping Array (Cta) Architecture, Originally Conceived By A Nasa Sponsored Team, Is A Very Promising New Technology. Not Only Has Cta Shown Outstanding Performance Metrics, But It Does So In A Manner That Is Scalable, Reliable And Offers Compact Stowage. The Proposed Innovation Is A Solar Array Design Consisting Of A Single Central Truss Structure Flanked By Tensioned Flexible Photovoltaic Blankets. This Configuration Has Been Shown In Multiple Analytical Studies To Be The Most Mass Efficient For A Cantilevered Solar Array. Phase I Results Confirm That Cta Has Very Low Structural Mass Which, With State-Of-Practice Cell Technology, Allows The Platform To Deliver Excellent Specific Power. For Example, Sub-200 Kw Systems Show Specific Power Approaching 190 W/Kg And Mega-Watt Versions Of Cta Still Produce Better Than 150 W/Kg. The Cta Stowed Wing Achieves The ?Compact? Attribute Due To The Fact That The Two Primary Components Of The System, The Boom And The Pv Blankets, Though By Different Methods, Both Stow Into Highly Volume-Efficient Packages. The Individual Boom Segments All Nest Neatly Inside One Another While The Pv Blankets Stow Into Compact Z-Folded Stacks. The Result Is A System That Is Capable Of Delivering Compactness In Excess Of 100 Kw/M?, Far Beyond Expectations. The Cta System, Although A New Solar Array Configuration, Is Shown Through Phase I Research To Have High Reliability. This Is Achieved By Leveraging Heritage Mechanical Subsystems And By Minimizing New Mechanism Design, Thereby Effectively Delivering A Higher Trl Than Would Ordinarily Be Associated With A New System. The Cta Design Draws Heavily From Heritage Designs Of Angstrom Designs Subcontractor Orbital Atk Goleta.
- 4 Jun 2018
- Igf::Ot::Igf Solar Arrays Power The Vast Majority Of Space Missions. Solar Arrays With Higher Power, Better Mass Efficiency And Improved Packaging Are Critical, Especially Given Nasa Interest In Solar Electric Propulsion (Sep). The Phase I Results Shows That The Compact Telescoping Array (Cta) Architecture, Originally Conceived By A Nasa Sponsored Team, Is A Very Promising New Technology. Not Only Has Cta Shown Outstanding Performance Metrics, But It Does So In A Manner That Is Scalable, Reliable And Offers Compact Stowage. The Proposed Innovation Is A Solar Array Design Consisting Of A Single Central Truss Structure Flanked By Tensioned Flexible Photovoltaic Blankets. This Configuration Has Been Shown In Multiple Analytical Studies To Be The Most Mass Efficient For A Cantilevered Solar Array. Phase I Results Confirm That Cta Has Very Low Structural Mass Which, With State-Of-Practice Cell Technology, Allows The Platform To Deliver Excellent Specific Power. For Example, Sub-200 Kw Systems Show Specific Power Approaching 190 W/Kg And Mega-Watt Versions Of Cta Still Produce Better Than 150 W/Kg. The Cta Stowed Wing Achieves The ?Compact? Attribute Due To The Fact That The Two Primary Components Of The System, The Boom And The Pv Blankets, Though By Different Methods, Both Stow Into Highly Volume-Efficient Packages. The Individual Boom Segments All Nest Neatly Inside One Another While The Pv Blankets Stow Into Compact Z-Folded Stacks. The Result Is A System That Is Capable Of Delivering Compactness In Excess Of 100 Kw/M?, Far Beyond Expectations. The Cta System, Although A New Solar Array Configuration, Is Shown Through Phase I Research To Have High Reliability. This Is Achieved By Leveraging Heritage Mechanical Subsystems And By Minimizing New Mechanism Design, Thereby Effectively Delivering A Higher Trl Than Would Ordinarily Be Associated With A New System. The Cta Design Draws Heavily From Heritage Designs Of Angstrom Designs Subcontractor Orbital Atk Goleta.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $748,952.00
- National Aeronautics And Space Administration (Nasa)
- FA881419C0009
- Update Section J Statement Of Work.
- 9 Jul 2020
- Update Section J Statement Of Work.
- Fa8814 Space Dev Test Plan Pkt La
- Department Of Defense (Dod)
- $1,999,121.00
- Department Of Defense (Dod)