SATPC0039601 Tab 04 4 SOW..pdf
PDF 147 KB Posted
- Attached to
- Cavitar Welding Camera Federal contract opportunity
- Solicitation number
- 80NSSC25913593Q
About this file
This Statement of Work (SOW) details NASA Marshall Space Flight Center's requirement for specialized Cavitar Welding Cameras. The procurement includes two specific camera models: the C400-B (Part Number A061) and the C350 HS (Part Number A048), each with unique technical specifications. The C400-B features 1140x1080 pixels, monochrome imaging at ~70fps, while the C350 HS offers 1440x1080 pixels with up to 500fps at 720x540 pixels. Both cameras are Class 3R laser systems and come with comprehensive accessories including power supplies, cables, cooling components, and installation software. Additional items include a heatsink for passive cooling and a thermally conductive sheet. The performance will take place at NASA Marshall Space Flight Center with a contract duration of 10-12 weeks.
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Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| SATPC0039601 Tab 04 QA Document.pdf | ||
| SATPC0039601 Tab 10 RFQ Open Market Template.pdf | ||
| SATPC0039601 Tab 06 BNJ..pdf |
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Text version
STATEMENT OF WORK
1. Objective/Requirements
NASA Marshall Space Flight Center has a requirement for the Cavitar Welding Cameras, the specifics are listed below.
2. Characteristics, Scope, and Specs
Description Part Number
QTY
Cavitar Welding Camera C400-B. Includes camera unit (1140x1080 pixels, monochrome, ~70fps at full resolution, max 100fps with 640nm laser illumination.) Power supply 24V DC with power cable, Adjustable working distance with hex key for adjustment, Gigabit Ethernet cable(10m), power cable & IO cable(10m), cooling hose connector with o-ring, hose clamp, spare protective window(plastic) and installation CD with Cavitar capture software. Classs 3R laser system.
A061 1
Cavitar Welding Camera C350 HS. Includes: Camera unit (1440x1080 pixels), monochrome, WD 150mm*, 200fps at full resolution, and up to 500fps at 720x540 pixels, power supply 24V and cable, USB 3.0 cable, camera power & IO cable (10m), cooling hose connector, hose clamp, spare protective window(plastic) and installation CD with Cavitar capture software. Class 3R laser system.
A048 1
Heatsink (2 pcs included for passive cooling at ambient temp up to ~35°C). Screws included
M115 1
Thermally conductive sheet (48mmx99mmx0,2mm). K023 1
3. Place of Performance NASA Marshall Space Flight Center
4. Period of Performance
10-12 weeks
File details come from the government source that posted it. Updated .