GraphitizationFurnace_QnA_20200618.docx

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Graphitization Furnace Federal contract opportunity
Solicitation number
80LARC20Q731649
Issued by
National Aeronautics and Space Administration Langley Research Center

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This document outlines a federal contract opportunity issued by the National Aeronautics and Space Administration Langley Research Center. The solicitation is for a graphitization furnace to process carbon composites at high temperatures, with specifications included as an attachment. Interested vendors must submit quotes by June 23rd addressing technical design, past performance, and price to be considered for award of a purchase order. The technical design must meet the temperature and size requirements, along with addressing site needs, schedule, and selection of a horizontal or vertical configuration. Past performance information on three relevant contracts is also required. Price quotes should include options for the base unit, training, and delivery. This requirement is set aside for small businesses under NAICS code 333994 for industrial process furnace manufacturing.

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FurnaceInstructionstoVendors.docx DOCX document
GraphitizationFurnaceSpecs.docx DOCX document

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Graphitization Furnace Questions and Answers

June 16, 2020 Q: We have been reviewing the solicitation and did not notice mention of a mass of the product to be cycled which would help in sizing the power supply.

A: Our estimate is that the part mass will be in the range of 60 kg retort with lots of room around it to about as much as a 130 kg solid part.

June 15, 2020 Q: What is the exact material they will be processing in it? They say a carbon based. We need a composition of the material used material cert.

A: Carbon composites. This is for materials research so we don’t have a specific material cert.

June 11, 2020 Vendor questions generated from market research and answers:

Q: Vendor asks NASA’s preference among a resistance heated furnace design operating at 2600°C or an induction heated furnace design reaching 2900°C.

A: NASA has a preference for the lowest cost design however we do desire the operating temperature to reach 2800°C.

Q: What is NASA’s current furnace set-up?

A: Our current high temperature system has a working hot zone of about 11 wide x 15 deep x 10 tall inches, Max temperature of 3000°C. Not certain on the power but think it is in the ballpark of 70 to 100 KW input.

Q: In what configuration are you looking for horizontal or vertical?

A: Either vertical or horizontal is fine, whatever is lower cost.

Q: Can the materials to be graphitized be loaded vertically?

A: We have no preference for vertical or horizontal load, and prefer the lowest cost option that meets the specifications.

Q: Do you expect to flow gas through the furnace, or just pull a deep vacuum even if it is multiple purge and vacuum cycles, to operate under partial pressure, or positive pressure?

A: We expect to purge the furnace with a continuous flow of inert gas while operational. Mass flow control is required. Typically these types of furnaces operate under a slight positive pressure, past systems have been about ¼ to ½ psig. We have not run this large of volume furnace before but our current systems operate at 1 or 2 liters per minute of purge gas during operation.

Q: I noted the pumping requirements which can certainly be achieved however if the plan is operate the system at the indicate level of vacuum the insulation package and hot zone will deteriorate faster than normal. If the vacuum is meant to be utilized at lower pressures (say below 2000°C) then it’s not an issue.

A: Vacuum is intended only for use in aiding the purging of the furnace of air, i.e. cycles of vacuum <100 torr back fill with inert gas. The furnace will not be operated under vacuum.

Q: For a system with this temperature I would assume a 3 phase system right off the bat.

A: Yes, we expect a three-phase system. 3 phase 460 Volts is typical in our laboratories. Higher voltage lines can be installed if required.

Q: Are there any material considerations that you cannot use?

A: Will be used for heating carbon-based materials; no special considerations for material construction that we are aware of.

Q: I am assuming you would have or would get the power needed for this system A: Yes, once we decide on a system, we will wire the laboratory to meet the power requirements.

Q: Please elaborate on “The final system design shall be approved by NASA Langley Research Center’s Information Technology Acquisition Management (ITAM) prior to contract award.”

A: ITAM may require copies of software from the selected vendor for testing prior to award. Their main concern is the compatibility and safety of IT (if any) that will interface with other NASA systems rather than the physical and functional aspects of the proposed furnace design.

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