SATPC0042356 TAB 07 SOW PRINTED.pdf

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Replacement hot zone parts for Thermal Technology high temperature furnace
Solicitation number
80NSSC26941350Q
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About this file

This is a Statement of Work for the Marshall Space Flight Center (MSFC) requiring custom replacement parts for a high-temperature furnace used in Space Nuclear Propulsion and shielding development research. The work is located in MSFC Building 4602, Room 1124.

The contractor must design and manufacture custom-fitted replacement components that are compatible with the existing high-temperature furnace system. Required deliverables include: a tungsten heating element (3.5" diameter, 8" long), a tungsten/molybdenum shield pack assembly, top hole shield assembly, bottom hole shield assembly, an arm shield pack (¾", tungsten/molybdenum), and a replacement o-ring kit. The contractor must also provide product details and installation instructions. These components are not commercial off-the-shelf products and must be specifically engineered to integrate with the existing furnace system at MSFC.

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STATEMENT OF WORK

1. Objective/Requirements The work done at MSFC on Space Nuclear Propulsion, shielding development, and other advanced materials areas requires a replacement tungsten heating element and tungsten/molybdenum heat shield for the high temperature furnace. The replacement parts are custom to the specific system and is NOT a commercial off the shelf product.

Therefore, the parts must be custom designed to fit this system. This system is currently located in MSFC building 4602 in room 1124.

2. Characteristics, Scope, and Specs

Requirements for the replacement heating element and heat shield are:

Must be manufactured to be compatible with our high temperature furnace

Tungsten/molybdenum shield pack assembly Top hole shield assembly Bottom hole shield assembly

Replacement o-ring kit

3. Requirement Documentation

Product details and installation instructions

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