SATPC0036385 Tab 04 4 SOW Updated.pdf

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Attached to
Purchase Request - Fuses for FLL Federal contract opportunity
Solicitation number
80NSSC24880812Q
Issued by
National Aeronautics and Space Administration Shared Services Center

About this file

This document is a Statement of Work (SOW) for a federal contract opportunity to procure time-delay fuses for use in the Flight Loads Lab (FLL) power control cabinets at the Armstrong Flight Research Center in Edwards, California.

The fuses must meet specific electrical and mechanical requirements, including voltage ratings of 600 VAC and 500 VDC, a current rating of 125 Amps, and an interrupting rating of 200 kA at 600 VAC and 20 kA at 500 VDC. The fuses must be new, unused, and meet UL Standard 248-8 Class J rating. A total of 170 fuses are required, with a delivery date of November 25, 2024. The related federal contract opportunity is solicitation number 80NSSC24880812Q, issued by the National Aeronautics and Space Administration Shared Services Center.

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Other files for this federal contract opportunity

Other files attached to Purchase Request - Fuses for FLL, newest first.
File Type Posted
SATPC0036385 Tab 04 4 SOW.pdf PDF
SATPC0036385 Tab 10 RFQ Open Market Template.pdf PDF
SATPC0036385 Tab 04 4 Specs.pdf PDF

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Text version

STATEMENT OF WORK

1. Objective/Requirements The Flight Loads Lab (FLL) need to procure time-delay fuses for use in its power control cabinets (PCCs) to support current and future operations of the lab in support of high-temperature thermal tests.

2. Characteristics, Scope, and Specs

The fuses shall not have been used in any applications prior to delivery.

The fuse shall be part number JTD-125 or one with equivalent electrical and mechanical characteristics, meeting the following specifications:

Electrical Requirements:

• Voltage ratings:

o 600 VAC o 500 VDC

• Current rating:

o 125 Amps

• Interrupting Rating:

o AC: 200 kA at 600 VAC o DC: 20 kA at 500 VDC

• Must meet UL Standard 248-8, Class J rating/approval o Must hold 500% of input current for a minimum of 10 seconds o Equivalent series: AJT, JTD, LPJ

Mechanical requirements

• Body style: Blade

• Fuse size: 5.75-inch Length x 1.5-inch diameter

• The fuse must have mechanical mounting points on each side that are between

108.7 mm and 113.5 mm apart.

3. Quantity needed: 170

4. Place of Performance

Armstrong Flight Research Center in Edwards, California.

5. Period of Performance/lead time The fuses shall be delivered by 25 November 2024.

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