SATPC0036337 Tab 04 4 SOW.pdf

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Attached to
Test leads, manifolds Federal contract opportunity
Solicitation number
80NSSC24880425Q
Issued by
National Aeronautics and Space Administration Shared Services Center

About this file

This document is a Statement of Work (SOW) for an investigation related to NASA's Explosive Transfer Line. The SOW lists the required hardware items, including couplers, manifolds, FCDC lines, TLX lines, and TLX test tips, along with the quantities and part numbers for each item. The vendor is also required to provide aerospace-grade confined detonating cord. The period of performance for the deliverables is estimated to be 24 months after the award. The payment milestones are structured in three phases, with the first phase covering the couplers and manifolds within 6 months, the second phase covering the TLX lines and TLX tips within 18 months, and the final phase covering the FCDC lines within 24 months. The hardware does not require flight certification or acceptance data packages.

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SATPC0036337 Tab 07 Capability Statement FBO Posting.pdf PDF

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Text version

STATEMENT OF WORK FOR NESC EXPLOSIVE TRANSFER LINE

INVESTIGATION

1.0 Scope

This Statement of work will cover the deliverables listed below from Collins Aerospace (Brand Name):

Line Item

Quantity Device Configuration/Notes

1 5 Coupler 1 input and 1 output. P/N: 81161-2 or equivalent that will mate with FCDC line and TLX line recommend 3/8 or ½ ports.

2 5 Manifold 1 input and 3 outputs. P/N 26280-3 or equivalent that will mate with FCDC line and TLX line recommend 3/8 or ½ ports.

3 10 FCDC Lines P/N: 7012300-01 or equivalent that will mate with the manifolds & couplers provided above recommend 3/8 or ½ connecting B-nuts.

4 10 TLX Lines P/N: 51912-143 or equivalent that will mate with the manifolds & couplers provided above recommend 3/8 or ½ connecting B-nuts.

5 20 TLX Test Tip P/N: 51674-5-0-394 or equivalent that will mate with the manifolds & couplers provided above recommend 3/8 or ½ connecting B-nuts.

The vendor shall supply aerospace grade confined detonating cord of approximately 2.5 grains per foot.

2.0 Data Deliverables

The hardware does not require flight certification or acceptance data packages.

3.0 Period of Performance

NASA is estimating a period of performance for Section 1.0 deliverables of this document to be complete 24 months after ATP.

4.0 Payment Milestones

Payment Milestone

Device(s) Estimated Period

1 Couplers Manifolds

NRE

6 months ARO

2 TLX Lines TLX Tips

18 months ARO

3 FCDC Lines 24 months ARO

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