SATPC0039144 Tab 04 4 SOW.pdf
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- Attached to
- COMPONENT (HIGH-POWER SCANNER WITH MOTORIZED COLLIMATOR IPG SCAN CONTROLLER), ETHERNET CAMERA, CAMERA ARM ASSEMBLY, MOTION INTERFACE BOARD, STANDARD SCAN HEAD CABLE KIT, PROTECTIVE WINDOW (D33 SERIES SCANNER), AND COMPONENT (YLR ADAPTER) Federal contract opportunity
- Solicitation number
- 80NSSC25907262Q
About this file
This Statement of Work (SOW) details NASA's requirement for specific high-precision scanning and imaging components to be delivered to the Marshall Space Flight Center. The procurement includes seven line items: a D33 3D High-Power Scanner with motorized collimator, an Ethernet camera (LUCID TRI016S), a horizontal camera arm assembly, a motion interface board, a standard scan head cable kit, a protective window for the D33 Series Scanner, and a YLR adapter. The equipment is specialized scientific instrumentation with precise technical specifications, such as a 500 mm focus lens, 1440 x 1080 resolution camera, and compatibility with 5V signal devices. The place of performance is NASA/Marshall Space Flight Center in Huntsville, Alabama, with a performance period of 4-6 weeks after receipt of order (ARO).
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Text version
STATEMENT OF WORK
1. Objective/Requirements
The information listed below is required to complete this purchase.
2. Characteristics, Scope, and Specs
LINE PART NO. DESCRIPTION QTY.
1 COMPONENT COMPONENT
CDSH0310PXDH31XU D33 3D High-Power Scanner with motorized collimator IPG Scan Controller, 24V (YLS/YLR) Laser Interface.
Vertical w/Camera option. 500 mm Focus Lens 100 mm collimator, HLC-8 connector.
2 CEMIXXX0002183PX Ethernet Camera - LUCID TRI016S
For through the lens visualization. Power over Ethernet Capable. 1440 x1080 Resolution. C-Mount. Grey Scale. PC Required.
3 P30-002424 Camera Arm Assembly, Horizontal, F125 (1x Mag)
Camera Arm, Ninety-degree (90°), 125 mm focal length.
4 CMUS1001478XXXXU Motion Interface Board
The motion interface is designed for use with 5V signal devices in typical applications involving gantries, linear stages, rotaries, encoder devices, or similar equipment.
5 CEU00005407X05XU Standard Scan Head Cable Kit, 5m
Recommended cable and connector kit for D33 2D High-Power
Scanner integrations that do not utilize an Integration Control Box. 5 meter scan head control and power cables provided.
6 COPWXXXXXXXX048U Protective Window, D33 Series Scanner (F500 SM)
Protective Window, D33 Series Scanner. For use with F500 SM lens.
7 COMPONENT COMPONENT
CEU00005478XXXXU YLR Adapter, M12 to HAN 24DD
3. Place of Performance
NASA/Marshall Space Flight Center
PS22-MCH
MSFC, AL 35812
United States
4. Period of Performance
4-6 weeks ARO
File details come from the government source that posted it. Updated .