Discovery Semiconductors, Inc.
CAGE Code: 0ZQE2
NCAGE Code: 0ZQE2
Status: Active
Type: Manufacturer
Dun & Bradstreet (DUNS): 824781769
Summary
Discovery Semiconductors, Inc. is an Active Manufacturer with the Cage Code 0ZQE2 and is tracked by Dun & Bradstreet under DUNS Number 824781769..
Address
119 Silvia St
Ewing NJ 08628-3200
United States
Points of Contact
- Telephone:
- 6094341311
- Fax:
- 6094341317
-
http://www.chipsat.com/
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Frequently Asked Questions (FAQ) for CAGE 0ZQE2
- What is CAGE Code 0ZQE2?
- 0ZQE2 is the unique identifier used by NATO Organizations to reference the physical entity known as Discovery Semiconductors, Inc. located at 119 Silvia St, Ewing NJ 08628-3200, United States.
- Who is CAGE Code 0ZQE2?
- 0ZQE2 refers to Discovery Semiconductors, Inc. located at 119 Silvia St, Ewing NJ 08628-3200, United States.
- Where is CAGE Code 0ZQE2 Located?
- CAGE Code 0ZQE2 is located in Ewing, NJ, USA.
Contracting History for CAGE 0ZQE2 Most Recent 25 Records
- 80NSSC19C0021
- Nasa Requires Five Variations Of Short-Wave Infrared (Swir) Ingaas Photodiode Subassemblies For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Mission. As Described In Nasa S Request For Proposal, Oci-Det-Sow-0067 And Oci-Det-Spec- 0015 Documents, The Primary Technical Challenge For These Ingaas Photodiodes Is To Achieve A Capacitance Less Than 11 Pf At Near Photovoltaic Operation With An Active Area Diameter Of 350 ?M. Such A Low Capacitance Device Requires An Ingaas Photodiode Structure Having A Capacitance Per Unit Area Of≪114 Pf / Mm2 At A Reverse Bias Of 100 Mv. Also, These Devices Must Withstand A Proton Radiation Up To A Fluence Level Of 2E10 / Cm2 For An Envisioned 3-Year Long Mission. These Photodiodes Must Be Integrated With Jfet Amplifiers In A Kovar Package, Both Supplied By Nasa Goddard Space Flight Center (Gsfc), To Manufacture Space-Qualified Photodiode Subassemblies. Discovery Semiconductors Submitted A Proposal, Titled Short-Wave Infrared Ingaas Photodiode For Optical Color Instrument (Oci) Of Pace Mission, On November 30, 2018. The Proposal Leveraged Our Prior Work In Developing Rad-Hard, Ultra-Low Noise, Large Area Ingaas Quadrant Photoreceivers For The Laser Interferometer Space Antenna (Lisa) Mission, To Manufacture The Pace Photodiode Flight Units. Nasa Reviewed Our Proposal And Suggested Splitting The Activities Into The Following Three Options For Budgetary Reasons: Option 1: Process 350 ?M Diameter Photodiode Chips, And Deliver 10 Chips In Die Form In A Gel-Pak. Option 2: Design And Manufacture (1) Photodiode Submount, (2) Motherboard Substrate, And (3) Container Needed To Develop The Photodiode Subassembly Flight Units. We Will Deliver 10 Photodiode Chips Mounted On Photodiode Submount And Motherboard Substrate. Option 3: Manufacture And Deliver 18 Photodiode Subassembly Flight Units And 18 Flight Spares With Supporting Documentation. Discovery Anticipates The Entire Effort To Be Funded And Will Perform The Various Technical Tasks As Described In Our Original Proposal Submitted On November 30, 2018. This Addendum Defines The Tasks Categorized According To The Three Options And The Corresponding Budget.
- 15 Dec 2020
- Nasa Requires Five Variations Of Short-Wave Infrared (Swir) Ingaas Photodiode Subassemblies For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Mission. As Described In Nasa S Request For Proposal, Oci-Det-Sow-0067 And Oci-Det-Spec- 0015 Documents, The Primary Technical Challenge For These Ingaas Photodiodes Is To Achieve A Capacitance Less Than 11 Pf At Near Photovoltaic Operation With An Active Area Diameter Of 350 ?M. Such A Low Capacitance Device Requires An Ingaas Photodiode Structure Having A Capacitance Per Unit Area Of≪114 Pf / Mm2 At A Reverse Bias Of 100 Mv. Also, These Devices Must Withstand A Proton Radiation Up To A Fluence Level Of 2E10 / Cm2 For An Envisioned 3-Year Long Mission. These Photodiodes Must Be Integrated With Jfet Amplifiers In A Kovar Package, Both Supplied By Nasa Goddard Space Flight Center (Gsfc), To Manufacture Space-Qualified Photodiode Subassemblies. Discovery Semiconductors Submitted A Proposal, Titled Short-Wave Infrared Ingaas Photodiode For Optical Color Instrument (Oci) Of Pace Mission, On November 30, 2018. The Proposal Leveraged Our Prior Work In Developing Rad-Hard, Ultra-Low Noise, Large Area Ingaas Quadrant Photoreceivers For The Laser Interferometer Space Antenna (Lisa) Mission, To Manufacture The Pace Photodiode Flight Units. Nasa Reviewed Our Proposal And Suggested Splitting The Activities Into The Following Three Options For Budgetary Reasons: Option 1: Process 350 ?M Diameter Photodiode Chips, And Deliver 10 Chips In Die Form In A Gel-Pak. Option 2: Design And Manufacture (1) Photodiode Submount, (2) Motherboard Substrate, And (3) Container Needed To Develop The Photodiode Subassembly Flight Units. We Will Deliver 10 Photodiode Chips Mounted On Photodiode Submount And Motherboard Substrate. Option 3: Manufacture And Deliver 18 Photodiode Subassembly Flight Units And 18 Flight Spares With Supporting Documentation. Discovery Anticipates The Entire Effort To Be Funded And Will Perform The Various Technical Tasks As Described In Our Original Proposal Submitted On November 30, 2018. This Addendum Defines The Tasks Categorized According To The Three Options And The Corresponding Budget.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $734,290.85
- National Aeronautics And Space Administration (Nasa)
- 80NSSC19C0021
- Nasa Requires Five Variations Of Short-Wave Infrared (Swir) Ingaas Photodiode Subassemblies For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Mission. As Described In Nasa S Request For Proposal, Oci-Det-Sow-0067 And Oci-Det-Spec- 0015 Documents, The Primary Technical Challenge For These Ingaas Photodiodes Is To Achieve A Capacitance Less Than 11 Pf At Near Photovoltaic Operation With An Active Area Diameter Of 350M. Such A Low Capacitance Device Requires An Ingaas Photodiode Structure Having A Capacitance Per Unit Area Of<114 Pf / Mm2 At A Reverse Bias Of 100 Mv. Also, These Devices Must Withstand A Proton Radiation Up To A Fluence Level Of 2E10 / Cm2 For An Envisioned 3-Year Long Mission. These Photodiodes Must Be Integrated With Jfet Amplifiers In A Kovar Package, Both Supplied By Nasa Goddard Space Flight Center (Gsfc), To Manufacture Space-Qualified Photodiode Subassemblies. Discovery Semiconductors Submitted A Proposal, Titled Short-Wave Infrared Ingaas Photodiode For Optical Color Instrument (Oci) Of Pace Mission, On November 30, 2018. The Proposal Leveraged Our Prior Work In Developing Rad-Hard, Ultra-Low Noise, Large Area Ingaas Quadrant Photoreceivers For The Laser Interferometer Space Antenna (Lisa) Mission, To Manufacture The Pace Photodiode Flight Units. Nasa Reviewed Our Proposal And Suggested Splitting The Activities Into The Following Three Options For Budgetary Reasons: Option 1: Process 350M Diameter Photodiode Chips, And Deliver 10 Chips In Die Form In A Gel-Pak. Option 2: Design And Manufacture (1) Photodiode Submount, (2) Motherboard Substrate, And (3) Container Needed To Develop The Photodiode Subassembly Flight Units. We Will Deliver 10 Photodiode Chips Mounted On Photodiode Submount And Motherboard Substrate. Option 3: Manufacture And Deliver 18 Photodiode Subassembly Flight Units And 18 Flight Spares With Supporting Documentation. Discovery Anticipates The Entire Effort To Be Funded And Will Perform The Various Technical Tasks As Described In Our Original Proposal Submitted On November 30, 2018. This Addendum Defines The Tasks Categorized According To The Three Options And The Corresponding Budget.
- 27 Mar 2019
- Nasa Requires Five Variations Of Short-Wave Infrared (Swir) Ingaas Photodiode Subassemblies For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Mission. As Described In Nasa S Request For Proposal, Oci-Det-Sow-0067 And Oci-Det-Spec- 0015 Documents, The Primary Technical Challenge For These Ingaas Photodiodes Is To Achieve A Capacitance Less Than 11 Pf At Near Photovoltaic Operation With An Active Area Diameter Of 350M. Such A Low Capacitance Device Requires An Ingaas Photodiode Structure Having A Capacitance Per Unit Area Of<114 Pf / Mm2 At A Reverse Bias Of 100 Mv. Also, These Devices Must Withstand A Proton Radiation Up To A Fluence Level Of 2E10 / Cm2 For An Envisioned 3-Year Long Mission. These Photodiodes Must Be Integrated With Jfet Amplifiers In A Kovar Package, Both Supplied By Nasa Goddard Space Flight Center (Gsfc), To Manufacture Space-Qualified Photodiode Subassemblies. Discovery Semiconductors Submitted A Proposal, Titled Short-Wave Infrared Ingaas Photodiode For Optical Color Instrument (Oci) Of Pace Mission, On November 30, 2018. The Proposal Leveraged Our Prior Work In Developing Rad-Hard, Ultra-Low Noise, Large Area Ingaas Quadrant Photoreceivers For The Laser Interferometer Space Antenna (Lisa) Mission, To Manufacture The Pace Photodiode Flight Units. Nasa Reviewed Our Proposal And Suggested Splitting The Activities Into The Following Three Options For Budgetary Reasons: Option 1: Process 350M Diameter Photodiode Chips, And Deliver 10 Chips In Die Form In A Gel-Pak. Option 2: Design And Manufacture (1) Photodiode Submount, (2) Motherboard Substrate, And (3) Container Needed To Develop The Photodiode Subassembly Flight Units. We Will Deliver 10 Photodiode Chips Mounted On Photodiode Submount And Motherboard Substrate. Option 3: Manufacture And Deliver 18 Photodiode Subassembly Flight Units And 18 Flight Spares With Supporting Documentation. Discovery Anticipates The Entire Effort To Be Funded And Will Perform The Various Technical Tasks As Described In Our Original Proposal Submitted On November 30, 2018. This Addendum Defines The Tasks Categorized According To The Three Options And The Corresponding Budget.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $479,926.85
- National Aeronautics And Space Administration (Nasa)
- 80NSSC19C0021
- Nasa Requires Five Variations Of Short-Wave Infrared (Swir) Ingaas Photodiode Subassemblies For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Mission. As Described In Nasa S Request For Proposal, Oci-Det-Sow-0067 And Oci-Det-Spec- 0015 Documents, The Primary Technical Challenge For These Ingaas Photodiodes Is To Achieve A Capacitance Less Than 11 Pf At Near Photovoltaic Operation With An Active Area Diameter Of 350 ?M. Such A Low Capacitance Device Requires An Ingaas Photodiode Structure Having A Capacitance Per Unit Area Of≪114 Pf / Mm2 At A Reverse Bias Of 100 Mv. Also, These Devices Must Withstand A Proton Radiation Up To A Fluence Level Of 2E10 / Cm2 For An Envisioned 3-Year Long Mission. These Photodiodes Must Be Integrated With Jfet Amplifiers In A Kovar Package, Both Supplied By Nasa Goddard Space Flight Center (Gsfc), To Manufacture Space-Qualified Photodiode Subassemblies. Discovery Semiconductors Submitted A Proposal, Titled Short-Wave Infrared Ingaas Photodiode For Optical Color Instrument (Oci) Of Pace Mission, On November 30, 2018. The Proposal Leveraged Our Prior Work In Developing Rad-Hard, Ultra-Low Noise, Large Area Ingaas Quadrant Photoreceivers For The Laser Interferometer Space Antenna (Lisa) Mission, To Manufacture The Pace Photodiode Flight Units. Nasa Reviewed Our Proposal And Suggested Splitting The Activities Into The Following Three Options For Budgetary Reasons: Option 1: Process 350 ?M Diameter Photodiode Chips, And Deliver 10 Chips In Die Form In A Gel-Pak. Option 2: Design And Manufacture (1) Photodiode Submount, (2) Motherboard Substrate, And (3) Container Needed To Develop The Photodiode Subassembly Flight Units. We Will Deliver 10 Photodiode Chips Mounted On Photodiode Submount And Motherboard Substrate. Option 3: Manufacture And Deliver 18 Photodiode Subassembly Flight Units And 18 Flight Spares With Supporting Documentation. Discovery Anticipates The Entire Effort To Be Funded And Will Perform The Various Technical Tasks As Described In Our Original Proposal Submitted On November 30, 2018. This Addendum Defines The Tasks Categorized According To The Three Options And The Corresponding Budget.
- 24 Jun 2020
- Nasa Requires Five Variations Of Short-Wave Infrared (Swir) Ingaas Photodiode Subassemblies For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Mission. As Described In Nasa S Request For Proposal, Oci-Det-Sow-0067 And Oci-Det-Spec- 0015 Documents, The Primary Technical Challenge For These Ingaas Photodiodes Is To Achieve A Capacitance Less Than 11 Pf At Near Photovoltaic Operation With An Active Area Diameter Of 350 ?M. Such A Low Capacitance Device Requires An Ingaas Photodiode Structure Having A Capacitance Per Unit Area Of≪114 Pf / Mm2 At A Reverse Bias Of 100 Mv. Also, These Devices Must Withstand A Proton Radiation Up To A Fluence Level Of 2E10 / Cm2 For An Envisioned 3-Year Long Mission. These Photodiodes Must Be Integrated With Jfet Amplifiers In A Kovar Package, Both Supplied By Nasa Goddard Space Flight Center (Gsfc), To Manufacture Space-Qualified Photodiode Subassemblies. Discovery Semiconductors Submitted A Proposal, Titled Short-Wave Infrared Ingaas Photodiode For Optical Color Instrument (Oci) Of Pace Mission, On November 30, 2018. The Proposal Leveraged Our Prior Work In Developing Rad-Hard, Ultra-Low Noise, Large Area Ingaas Quadrant Photoreceivers For The Laser Interferometer Space Antenna (Lisa) Mission, To Manufacture The Pace Photodiode Flight Units. Nasa Reviewed Our Proposal And Suggested Splitting The Activities Into The Following Three Options For Budgetary Reasons: Option 1: Process 350 ?M Diameter Photodiode Chips, And Deliver 10 Chips In Die Form In A Gel-Pak. Option 2: Design And Manufacture (1) Photodiode Submount, (2) Motherboard Substrate, And (3) Container Needed To Develop The Photodiode Subassembly Flight Units. We Will Deliver 10 Photodiode Chips Mounted On Photodiode Submount And Motherboard Substrate. Option 3: Manufacture And Deliver 18 Photodiode Subassembly Flight Units And 18 Flight Spares With Supporting Documentation. Discovery Anticipates The Entire Effort To Be Funded And Will Perform The Various Technical Tasks As Described In Our Original Proposal Submitted On November 30, 2018. This Addendum Defines The Tasks Categorized According To The Three Options And The Corresponding Budget.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $988,655.97
- National Aeronautics And Space Administration (Nasa)
- 80NSSC19C0021
- Nasa Requires Five Variations Of Short-Wave Infrared (Swir) Ingaas Photodiode Subassemblies For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Mission. As Described In Nasa S Request For Proposal, Oci-Det-Sow-0067 And Oci-Det-Spec- 0015 Documents, The Primary Technical Challenge For These Ingaas Photodiodes Is To Achieve A Capacitance Less Than 11 Pf At Near Photovoltaic Operation With An Active Area Diameter Of 350 ?M. Such A Low Capacitance Device Requires An Ingaas Photodiode Structure Having A Capacitance Per Unit Area Of≪114 Pf / Mm2 At A Reverse Bias Of 100 Mv. Also, These Devices Must Withstand A Proton Radiation Up To A Fluence Level Of 2E10 / Cm2 For An Envisioned 3-Year Long Mission. These Photodiodes Must Be Integrated With Jfet Amplifiers In A Kovar Package, Both Supplied By Nasa Goddard Space Flight Center (Gsfc), To Manufacture Space-Qualified Photodiode Subassemblies. Discovery Semiconductors Submitted A Proposal, Titled Short-Wave Infrared Ingaas Photodiode For Optical Color Instrument (Oci) Of Pace Mission, On November 30, 2018. The Proposal Leveraged Our Prior Work In Developing Rad-Hard, Ultra-Low Noise, Large Area Ingaas Quadrant Photoreceivers For The Laser Interferometer Space Antenna (Lisa) Mission, To Manufacture The Pace Photodiode Flight Units. Nasa Reviewed Our Proposal And Suggested Splitting The Activities Into The Following Three Options For Budgetary Reasons: Option 1: Process 350 ?M Diameter Photodiode Chips, And Deliver 10 Chips In Die Form In A Gel-Pak. Option 2: Design And Manufacture (1) Photodiode Submount, (2) Motherboard Substrate, And (3) Container Needed To Develop The Photodiode Subassembly Flight Units. We Will Deliver 10 Photodiode Chips Mounted On Photodiode Submount And Motherboard Substrate. Option 3: Manufacture And Deliver 18 Photodiode Subassembly Flight Units And 18 Flight Spares With Supporting Documentation. Discovery Anticipates The Entire Effort To Be Funded And Will Perform The Various Technical Tasks As Described In Our Original Proposal Submitted On November 30, 2018. This Addendum Defines The Tasks Categorized According To The Three Options And The Corresponding Budget.
- 19 Mar 2020
- Nasa Requires Five Variations Of Short-Wave Infrared (Swir) Ingaas Photodiode Subassemblies For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Mission. As Described In Nasa S Request For Proposal, Oci-Det-Sow-0067 And Oci-Det-Spec- 0015 Documents, The Primary Technical Challenge For These Ingaas Photodiodes Is To Achieve A Capacitance Less Than 11 Pf At Near Photovoltaic Operation With An Active Area Diameter Of 350 ?M. Such A Low Capacitance Device Requires An Ingaas Photodiode Structure Having A Capacitance Per Unit Area Of≪114 Pf / Mm2 At A Reverse Bias Of 100 Mv. Also, These Devices Must Withstand A Proton Radiation Up To A Fluence Level Of 2E10 / Cm2 For An Envisioned 3-Year Long Mission. These Photodiodes Must Be Integrated With Jfet Amplifiers In A Kovar Package, Both Supplied By Nasa Goddard Space Flight Center (Gsfc), To Manufacture Space-Qualified Photodiode Subassemblies. Discovery Semiconductors Submitted A Proposal, Titled Short-Wave Infrared Ingaas Photodiode For Optical Color Instrument (Oci) Of Pace Mission, On November 30, 2018. The Proposal Leveraged Our Prior Work In Developing Rad-Hard, Ultra-Low Noise, Large Area Ingaas Quadrant Photoreceivers For The Laser Interferometer Space Antenna (Lisa) Mission, To Manufacture The Pace Photodiode Flight Units. Nasa Reviewed Our Proposal And Suggested Splitting The Activities Into The Following Three Options For Budgetary Reasons: Option 1: Process 350 ?M Diameter Photodiode Chips, And Deliver 10 Chips In Die Form In A Gel-Pak. Option 2: Design And Manufacture (1) Photodiode Submount, (2) Motherboard Substrate, And (3) Container Needed To Develop The Photodiode Subassembly Flight Units. We Will Deliver 10 Photodiode Chips Mounted On Photodiode Submount And Motherboard Substrate. Option 3: Manufacture And Deliver 18 Photodiode Subassembly Flight Units And 18 Flight Spares With Supporting Documentation. Discovery Anticipates The Entire Effort To Be Funded And Will Perform The Various Technical Tasks As Described In Our Original Proposal Submitted On November 30, 2018. This Addendum Defines The Tasks Categorized According To The Three Options And The Corresponding Budget.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $988,655.97
- National Aeronautics And Space Administration (Nasa)
- 80NSSC20P1661
- Pn Dsc-R212-89-Fc/Apc-G-2 10Plus Ghz Linear Agc Balanced, Uncooled 2.2 Micron Wavelength Pin Photoreceiver
- 28 Jul 2020
- Pn Dsc-R212-89-Fc/Apc-G-2 10Plus Ghz Linear Agc Balanced, Uncooled 2.2 Micron Wavelength Pin Photoreceiver
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $15,100.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC19C0021
- Nasa Requires Five Variations Of Short-Wave Infrared (Swir) Ingaas Photodiode Subassemblies For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Mission. As Described In Nasa S Request For Proposal, Oci-Det-Sow-0067 And Oci-Det-Spec- 0015 Documents, The Primary Technical Challenge For These Ingaas Photodiodes Is To Achieve A Capacitance Less Than 11 Pf At Near Photovoltaic Operation With An Active Area Diameter Of 350M. Such A Low Capacitance Device Requires An Ingaas Photodiode Structure Having A Capacitance Per Unit Area Of<114 Pf / Mm2 At A Reverse Bias Of 100 Mv. Also, These Devices Must Withstand A Proton Radiation Up To A Fluence Level Of 2E10 / Cm2 For An Envisioned 3-Year Long Mission. These Photodiodes Must Be Integrated With Jfet Amplifiers In A Kovar Package, Both Supplied By Nasa Goddard Space Flight Center (Gsfc), To Manufacture Space-Qualified Photodiode Subassemblies. Discovery Semiconductors Submitted A Proposal, Titled Short-Wave Infrared Ingaas Photodiode For Optical Color Instrument (Oci) Of Pace Mission, On November 30, 2018. The Proposal Leveraged Our Prior Work In Developing Rad-Hard, Ultra-Low Noise, Large Area Ingaas Quadrant Photoreceivers For The Laser Interferometer Space Antenna (Lisa) Mission, To Manufacture The Pace Photodiode Flight Units. Nasa Reviewed Our Proposal And Suggested Splitting The Activities Into The Following Three Options For Budgetary Reasons: Option 1: Process 350M Diameter Photodiode Chips, And Deliver 10 Chips In Die Form In A Gel-Pak. Option 2: Design And Manufacture (1) Photodiode Submount, (2) Motherboard Substrate, And (3) Container Needed To Develop The Photodiode Subassembly Flight Units. We Will Deliver 10 Photodiode Chips Mounted On Photodiode Submount And Motherboard Substrate. Option 3: Manufacture And Deliver 18 Photodiode Subassembly Flight Units And 18 Flight Spares With Supporting Documentation. Discovery Anticipates The Entire Effort To Be Funded And Will Perform The Various Technical Tasks As Described In Our Original Proposal Submitted On November 30, 2018. This Addendum Defines The Tasks Categorized According To The Three Options And The Corresponding Budget.
- 25 Jun 2019
- Nasa Requires Five Variations Of Short-Wave Infrared (Swir) Ingaas Photodiode Subassemblies For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Mission. As Described In Nasa S Request For Proposal, Oci-Det-Sow-0067 And Oci-Det-Spec- 0015 Documents, The Primary Technical Challenge For These Ingaas Photodiodes Is To Achieve A Capacitance Less Than 11 Pf At Near Photovoltaic Operation With An Active Area Diameter Of 350M. Such A Low Capacitance Device Requires An Ingaas Photodiode Structure Having A Capacitance Per Unit Area Of<114 Pf / Mm2 At A Reverse Bias Of 100 Mv. Also, These Devices Must Withstand A Proton Radiation Up To A Fluence Level Of 2E10 / Cm2 For An Envisioned 3-Year Long Mission. These Photodiodes Must Be Integrated With Jfet Amplifiers In A Kovar Package, Both Supplied By Nasa Goddard Space Flight Center (Gsfc), To Manufacture Space-Qualified Photodiode Subassemblies. Discovery Semiconductors Submitted A Proposal, Titled Short-Wave Infrared Ingaas Photodiode For Optical Color Instrument (Oci) Of Pace Mission, On November 30, 2018. The Proposal Leveraged Our Prior Work In Developing Rad-Hard, Ultra-Low Noise, Large Area Ingaas Quadrant Photoreceivers For The Laser Interferometer Space Antenna (Lisa) Mission, To Manufacture The Pace Photodiode Flight Units. Nasa Reviewed Our Proposal And Suggested Splitting The Activities Into The Following Three Options For Budgetary Reasons: Option 1: Process 350M Diameter Photodiode Chips, And Deliver 10 Chips In Die Form In A Gel-Pak. Option 2: Design And Manufacture (1) Photodiode Submount, (2) Motherboard Substrate, And (3) Container Needed To Develop The Photodiode Subassembly Flight Units. We Will Deliver 10 Photodiode Chips Mounted On Photodiode Submount And Motherboard Substrate. Option 3: Manufacture And Deliver 18 Photodiode Subassembly Flight Units And 18 Flight Spares With Supporting Documentation. Discovery Anticipates The Entire Effort To Be Funded And Will Perform The Various Technical Tasks As Described In Our Original Proposal Submitted On November 30, 2018. This Addendum Defines The Tasks Categorized According To The Three Options And The Corresponding Budget.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $479,926.85
- National Aeronautics And Space Administration (Nasa)
- N0017319P0779
- Photodiodes Pr# 56-9506-19
- 10 Apr 2019
- Photodiodes Pr# 56-9506-19
- Naval Research Laboratory
- Department Of Defense (Dod)
- $30,875.00
- Department Of Defense (Dod)
- 80NSSC19C0021
- Nasa Requires Five Variations Of Short-Wave Infrared (Swir) Ingaas Photodiode Subassemblies For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Mission. As Described In Nasa S Request For Proposal, Oci-Det-Sow-0067 And Oci-Det-Spec- 0015 Documents, The Primary Technical Challenge For These Ingaas Photodiodes Is To Achieve A Capacitance Less Than 11 Pf At Near Photovoltaic Operation With An Active Area Diameter Of 350 ?M. Such A Low Capacitance Device Requires An Ingaas Photodiode Structure Having A Capacitance Per Unit Area Of≪114 Pf / Mm2 At A Reverse Bias Of 100 Mv. Also, These Devices Must Withstand A Proton Radiation Up To A Fluence Level Of 2E10 / Cm2 For An Envisioned 3-Year Long Mission. These Photodiodes Must Be Integrated With Jfet Amplifiers In A Kovar Package, Both Supplied By Nasa Goddard Space Flight Center (Gsfc), To Manufacture Space-Qualified Photodiode Subassemblies. Discovery Semiconductors Submitted A Proposal, Titled Short-Wave Infrared Ingaas Photodiode For Optical Color Instrument (Oci) Of Pace Mission, On November 30, 2018. The Proposal Leveraged Our Prior Work In Developing Rad-Hard, Ultra-Low Noise, Large Area Ingaas Quadrant Photoreceivers For The Laser Interferometer Space Antenna (Lisa) Mission, To Manufacture The Pace Photodiode Flight Units. Nasa Reviewed Our Proposal And Suggested Splitting The Activities Into The Following Three Options For Budgetary Reasons: Option 1: Process 350 ?M Diameter Photodiode Chips, And Deliver 10 Chips In Die Form In A Gel-Pak. Option 2: Design And Manufacture (1) Photodiode Submount, (2) Motherboard Substrate, And (3) Container Needed To Develop The Photodiode Subassembly Flight Units. We Will Deliver 10 Photodiode Chips Mounted On Photodiode Submount And Motherboard Substrate. Option 3: Manufacture And Deliver 18 Photodiode Subassembly Flight Units And 18 Flight Spares With Supporting Documentation. Discovery Anticipates The Entire Effort To Be Funded And Will Perform The Various Technical Tasks As Described In Our Original Proposal Submitted On November 30, 2018. This Addendum Defines The Tasks Categorized According To The Three Options And The Corresponding Budget.
- 27 Mar 2019
- Nasa Requires Five Variations Of Short-Wave Infrared (Swir) Ingaas Photodiode Subassemblies For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Mission. As Described In Nasa S Request For Proposal, Oci-Det-Sow-0067 And Oci-Det-Spec- 0015 Documents, The Primary Technical Challenge For These Ingaas Photodiodes Is To Achieve A Capacitance Less Than 11 Pf At Near Photovoltaic Operation With An Active Area Diameter Of 350 ?M. Such A Low Capacitance Device Requires An Ingaas Photodiode Structure Having A Capacitance Per Unit Area Of≪114 Pf / Mm2 At A Reverse Bias Of 100 Mv. Also, These Devices Must Withstand A Proton Radiation Up To A Fluence Level Of 2E10 / Cm2 For An Envisioned 3-Year Long Mission. These Photodiodes Must Be Integrated With Jfet Amplifiers In A Kovar Package, Both Supplied By Nasa Goddard Space Flight Center (Gsfc), To Manufacture Space-Qualified Photodiode Subassemblies. Discovery Semiconductors Submitted A Proposal, Titled Short-Wave Infrared Ingaas Photodiode For Optical Color Instrument (Oci) Of Pace Mission, On November 30, 2018. The Proposal Leveraged Our Prior Work In Developing Rad-Hard, Ultra-Low Noise, Large Area Ingaas Quadrant Photoreceivers For The Laser Interferometer Space Antenna (Lisa) Mission, To Manufacture The Pace Photodiode Flight Units. Nasa Reviewed Our Proposal And Suggested Splitting The Activities Into The Following Three Options For Budgetary Reasons: Option 1: Process 350 ?M Diameter Photodiode Chips, And Deliver 10 Chips In Die Form In A Gel-Pak. Option 2: Design And Manufacture (1) Photodiode Submount, (2) Motherboard Substrate, And (3) Container Needed To Develop The Photodiode Subassembly Flight Units. We Will Deliver 10 Photodiode Chips Mounted On Photodiode Submount And Motherboard Substrate. Option 3: Manufacture And Deliver 18 Photodiode Subassembly Flight Units And 18 Flight Spares With Supporting Documentation. Discovery Anticipates The Entire Effort To Be Funded And Will Perform The Various Technical Tasks As Described In Our Original Proposal Submitted On November 30, 2018. This Addendum Defines The Tasks Categorized According To The Three Options And The Corresponding Budget.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $988,655.97
- National Aeronautics And Space Administration (Nasa)
- N6600121P6563
- Balanced Pin Photodiodes To 16+Ghz
- 25 Aug 2021
- Balanced Pin Photodiodes To 16+Ghz
- Niwc Pacific
- Department Of Defense (Dod)
- $157,600.00
- Department Of Defense (Dod)
- N0017319P0110
- Photodiode/Antenna Pr# 56-9544-18
- 22 Oct 2018
- Photodiode/Antenna Pr# 56-9544-18
- Naval Research Laboratory
- Department Of Defense (Dod)
- $24,600.00
- Department Of Defense (Dod)
- FA875119PA154
- Ingaas Pin Photodiode
- 9 Sep 2019
- Ingaas Pin Photodiode
- Fa8751 Afrl Riko
- Department Of Defense (Dod)
- $20,600.00
- Department Of Defense (Dod)
- N0017323P6007
- Dsc100s-39-Fc/Apc-Sma-1
- 19 Jul 2023
- Dsc100s-39-Fc/Apc-Sma-1
- Naval Research Laboratory
- Department Of Defense (Dod)
- $29,000.00
- Department Of Defense (Dod)
- N0016417P0602
- Photodetector
- 12 Sep 2017
- Photodetector
- Nswc Crane
- Department Of Defense (Dod)
- $41,140.00
- Department Of Defense (Dod)
- 80NSSC18P3731
- Dsc-R413-1-C
- 28 Sep 2018
- Dsc-R413-1-C
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $50,075.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC19C0021
- Nasa Requires Five Variations Of Short-Wave Infrared (Swir) Ingaas Photodiode Subassemblies For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Mission. As Described In Nasa S Request For Proposal, Oci-Det-Sow-0067 And Oci-Det-Spec- 0015 Documents, The Primary Technical Challenge For These Ingaas Photodiodes Is To Achieve A Capacitance Less Than 11 Pf At Near Photovoltaic Operation With An Active Area Diameter Of 350 ?M. Such A Low Capacitance Device Requires An Ingaas Photodiode Structure Having A Capacitance Per Unit Area Of≪114 Pf / Mm2 At A Reverse Bias Of 100 Mv. Also, These Devices Must Withstand A Proton Radiation Up To A Fluence Level Of 2E10 / Cm2 For An Envisioned 3-Year Long Mission. These Photodiodes Must Be Integrated With Jfet Amplifiers In A Kovar Package, Both Supplied By Nasa Goddard Space Flight Center (Gsfc), To Manufacture Space-Qualified Photodiode Subassemblies. Discovery Semiconductors Submitted A Proposal, Titled Short-Wave Infrared Ingaas Photodiode For Optical Color Instrument (Oci) Of Pace Mission, On November 30, 2018. The Proposal Leveraged Our Prior Work In Developing Rad-Hard, Ultra-Low Noise, Large Area Ingaas Quadrant Photoreceivers For The Laser Interferometer Space Antenna (Lisa) Mission, To Manufacture The Pace Photodiode Flight Units. Nasa Reviewed Our Proposal And Suggested Splitting The Activities Into The Following Three Options For Budgetary Reasons: Option 1: Process 350 ?M Diameter Photodiode Chips, And Deliver 10 Chips In Die Form In A Gel-Pak. Option 2: Design And Manufacture (1) Photodiode Submount, (2) Motherboard Substrate, And (3) Container Needed To Develop The Photodiode Subassembly Flight Units. We Will Deliver 10 Photodiode Chips Mounted On Photodiode Submount And Motherboard Substrate. Option 3: Manufacture And Deliver 18 Photodiode Subassembly Flight Units And 18 Flight Spares With Supporting Documentation. Discovery Anticipates The Entire Effort To Be Funded And Will Perform The Various Technical Tasks As Described In Our Original Proposal Submitted On November 30, 2018. This Addendum Defines The Tasks Categorized According To The Three Options And The Corresponding Budget.
- 9 Oct 2020
- Nasa Requires Five Variations Of Short-Wave Infrared (Swir) Ingaas Photodiode Subassemblies For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Mission. As Described In Nasa S Request For Proposal, Oci-Det-Sow-0067 And Oci-Det-Spec- 0015 Documents, The Primary Technical Challenge For These Ingaas Photodiodes Is To Achieve A Capacitance Less Than 11 Pf At Near Photovoltaic Operation With An Active Area Diameter Of 350 ?M. Such A Low Capacitance Device Requires An Ingaas Photodiode Structure Having A Capacitance Per Unit Area Of≪114 Pf / Mm2 At A Reverse Bias Of 100 Mv. Also, These Devices Must Withstand A Proton Radiation Up To A Fluence Level Of 2E10 / Cm2 For An Envisioned 3-Year Long Mission. These Photodiodes Must Be Integrated With Jfet Amplifiers In A Kovar Package, Both Supplied By Nasa Goddard Space Flight Center (Gsfc), To Manufacture Space-Qualified Photodiode Subassemblies. Discovery Semiconductors Submitted A Proposal, Titled Short-Wave Infrared Ingaas Photodiode For Optical Color Instrument (Oci) Of Pace Mission, On November 30, 2018. The Proposal Leveraged Our Prior Work In Developing Rad-Hard, Ultra-Low Noise, Large Area Ingaas Quadrant Photoreceivers For The Laser Interferometer Space Antenna (Lisa) Mission, To Manufacture The Pace Photodiode Flight Units. Nasa Reviewed Our Proposal And Suggested Splitting The Activities Into The Following Three Options For Budgetary Reasons: Option 1: Process 350 ?M Diameter Photodiode Chips, And Deliver 10 Chips In Die Form In A Gel-Pak. Option 2: Design And Manufacture (1) Photodiode Submount, (2) Motherboard Substrate, And (3) Container Needed To Develop The Photodiode Subassembly Flight Units. We Will Deliver 10 Photodiode Chips Mounted On Photodiode Submount And Motherboard Substrate. Option 3: Manufacture And Deliver 18 Photodiode Subassembly Flight Units And 18 Flight Spares With Supporting Documentation. Discovery Anticipates The Entire Effort To Be Funded And Will Perform The Various Technical Tasks As Described In Our Original Proposal Submitted On November 30, 2018. This Addendum Defines The Tasks Categorized According To The Three Options And The Corresponding Budget.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $988,655.97
- National Aeronautics And Space Administration (Nasa)
- N0017323P6007
- Dsc100s-39-Fc/Apc-Sma-1
- 27 Sep 2023
- Dsc100s-39-Fc/Apc-Sma-1
- Naval Research Laboratory
- Department Of Defense (Dod)
- $29,000.00
- Department Of Defense (Dod)