Tab 04 SOW.pdf
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- Attached to
- 16-Channel 28144 Quad Bridge Conditioner System Federal contract opportunity
- Solicitation number
- 80NSSC26940463Q
About this file
This is a Statement of Work for a Precision 16-Channel 28144 Quad Bridge Conditioner System with Test Subsystem required by NASA Langley Research Center. The system configuration consists of 12 line items totaling specific quantities of hardware and assembly services. Key components include a 16-slot chassis (28016F-M3) with power supply, a backplane interface module with Ethernet remote interface and Windows-based GUI software, four quad bridge/dynamic strain conditioner cards with 8-pole low-pass filters, output cables, a 64-channel BNC bulkhead panel for standard 19-inch rack mount, factory assembly services for cable and panel integration, and test subsystem instruments including Keysight 33509B and 34465A equipment with associated cables and rack mount hardware. One test cable for Factory Acceptance Testing (FAT) on cards is also included.
Performance of work is to be completed at NASA Langley Research Center in Hampton, Virginia, Building 1221B, Room 144, with point of contact Neal Haas. The period of performance is 60-90 days as requested. The Statement of Work establishes the specific technical requirements and deliverables but does not address pricing terms, response deadlines, award dates, or contract vehicle information.
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| File | Type | Posted |
|---|---|---|
| Tab 07 Capability Statement.pdf |
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Text version
STATEMENT OF WORK
1. Objective/Requirements
NASA Langley Research Center has a requirement for a Precision 16-Channel 28144 Quad Bridge Conditioner System with Test Subsystem
2. Characteristics, Scope, and Specs
Precision 16-Channel 28144 Quad Bridge Conditioner System with Test Subsystem
Configuration:
LINE PART NO. DESCRIPTION QTY.
1 28016F-M3 28016F-M3 16-Slot Chassis with Four 50-Pin D Output Connectors at the Rear Panel
2 28016C 28016C -ACPS-1 Power Supply for 28016 Mainframe, 115 VAC
3 28000A-BIF2-FT Backplane Interface Module with Ethernet Remote Interface.
Windows-based GUI software is included. With Option F, FAT/GNG test support.
4 28000-BP-1A 28000 Frame Blank Panel, 1 Card Slot
5 28000-BP-2A 28000 Frame Blank Panel, 2 Card Slots
6 28000-BP-4A 28000 Frame Blank Panel, 4 Card Slots
7 28144-LP8FP-L Quad Bridge/Dyn. Strain Conditioner, with 8-Pole Low- Pass Filters. With Option L, Transducer Leakage Resistance Measurement Support in constant current excitation mode.
8 CB-DD50P/16BNCF-BH-4 Output Cable. DD50P to 16- Channel BNC Female Output for Bulkhead Panel Mount, 4-foot length. Used for Quad Channel Card Outputs.
9 PNL-64BNCBH-3U Panel for 64 Bulkhead Mounted BNC's, Standard 19-inch Rack Mount, 5.25-inch Height (3U).
Labelled 0-63.
10 N/A Factory Assembly Right to Left
– Assemble Qty 4 cables (line 8) into panel (Item 9) Connector channel numbers labeled right to left in ascending order.
11 28000-5-TEST Test Subsystem Instruments (Keysight 33509B and 34465A) and Cables for use with 28000A- BIF2-FT and 28000 chassis.
Includes rack mount hardware, monitor bus cable and test bus BNC cable.
12 CB-REF-C Test Cable for performing FAT on cards in "M3" Chassis
3. Place of Performance
NASA Langley Research Center (LaRC) ATTN: Neal Haas, Building #: 1221B, Room #: 144 Hampton VA 23681-2199
4. Period of Performance
60-90 days ARO.
File details come from the government source that posted it. Updated .