Site Visit Questions and Answers.pdf
PDF 79 KB Posted
- Attached to
- Composite Processing Ovens Federal contract opportunity
- Solicitation number
- FA8125-22-Q-0059
About this file
This document contains a solicitation for composite processing ovens and details regarding an associated site visit. The solicitation number is FA8125-22-Q-0059 and is seeking proposals for composite processing ovens to be used at an Air Force facility. Interested parties must RSVP for the mandatory site visit scheduled on April 5th, 2022 between 10AM and 12PM by notifying Sheridan Robison at the provided email address with attendee information by March 30th, 2022 at 10AM. The site visit will be held on an Air Force installation and valid identification will be required for entry. Electronic submission of proposals through FedBizOps is required, with no phone inquiries accepted. The point of contact for any further questions is the contracting officer, Sheridan Robison. The soliciting agency is the Department of the Air Force Materiel Command Air Force Sustainment Center.
View the file
Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| Solicitation Amendment FA812522Q00590002 SF 30.pdf | ||
| Revision 3 - SOW for Composite Processing Ovens.pdf | ||
| Solicitation Amendment FA812522Q00590001 SF 30.pdf | ||
| Solicitation - FA812522Q0059.pdf | ||
| Site Visit.pdf | ||
| Statement of Work for Composite Processing Ovens.pdf |
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Text version
Question 1: Will the system be qualified based on part temperature or air temp?
Answer 1: The system will be qualified on the TUS and SAT in an empty oven per AMS 2750.
Also we would like to add a test with a few of our E-3 radomes at once. One radome is roughly (LxHxW) 48”x57”x74” 75lbs. The stands they are on are roughly 20lbs. The nose radome is of sandwich construction. The honeycomb core is 3/16 cell 0.252 thick with four pounds per cubic foot density. The core is fiberglass fabric reinforced phenolic resin. The core is faced on the interior and exterior surface with four plies of style 181 fiberglass fabric reinforced epoxy resin.
The AFT edge is reinforced with filler plies for structural attachment. The external surface is finished with erosion resistant white astrocoat.
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