SATPC0037127 TAB 04 4 SOW.pdf

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UT24CP1008 CertusPro-NX-RT Field Programmable Gate Array (FPGA), Mixed I/O voltage (1. 2V - 3. 3V), Space PEM QD flow; packaged in a 484 lead (SnPb) plastic ball grid array, specified at -40oC to +125oC junction temperature. Radiation hardness 100krad (Si).
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80NSSC25886514Q
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This Statement of Work outlines NASA Search & Rescue Office's requirements for five (5) UT24CP1008RBLA CertusPro-NX-RT Field Programmable Gate Arrays (FPGAs) for use in low-cost, space-rated, radiation-tolerant search and rescue receiver and beacon transmitter research and development.

The FPGAs must meet specific technical requirements including 19mm x 19mm chip dimensions, 0.8mm ball pitch, 484 lead plastic ball grid array, speed grade of 8, 96k logic cells, radiation hardness of 100 krad(Si), and operational temperature range of -30°C to +70°C with space/automotive level temperature screening from -40°C to +125°C. The items will be commercial-off-the-shelf (COTS) components for use at NASA Goddard Spaceflight Center (GSFC), with the period of performance spanning from purchase placement through receipt.

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STATEMENT OF WORK FOR FIVE (5) FIELD GATE PROGRAMMABLE ARRAYS

1. Objective/Requirements The NASA Search & Rescue Office requires quantity five (5) field-gate programmable array (FPGA) electronics subcomponents / chips. These FGPAs will be used for low-cost, space-rated, radiation-tolerant search and rescue (SAR) receiver and SAR beacon transmitter research and development. The items to be purchased are UT24CP1008RBLA CertusPro-NX-RT Field Programmable Gate Arrays (FPGAs) based on NASA’s requirements specified in section 2 – Characteristics, Scope and Specs.

2. Characteristics, Scope, and Specs

The FPGAs shall have the following characteristics:

- Physical o Chip Dimension: 19 mm × 19 mm o Ball Pitch: 0.8 mm o Ball Grid Array Size: 484 lead (SnPb) plastic ball grid array

- Performance o Speed Grade: 8 o Logic Cell Count: 96k Logic Cells

- Space/Operational Environment Rating o Radiation Hardness: 100 krad(Si) o Temperature Range: -30°C to +70°C

- Component Screening o Temperature Screening: Space / Automotive level (-40°C to +125°C)

3. Place of Performance Non-applicable, item shall be a commercial-off-the-shelf (COTS) item for use in a workspace environment at NASA Goddard Spaceflight Center (GSFC.

4. Period of Performance Purchase placement through receipt of item.

File details come from the government source that posted it. Updated .