Attachment 1_ Detailed Design.pdf
PDF 2 MB Posted
- Solicitation number
- FA700020Q0075
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Other files
| File | Type | Posted |
|---|---|---|
| Attachment 2 Design details.pdf | ||
| updated Sources Sought for windtunnel appliance.docx | DOCX document | |
| Sources Sought windtunnel nozzle.docx | DOCX document |
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Text version
List of drawings
LT-USAFA-1.01.01.00 Ludwieg Tube, total view
LT-USAFA-1.02.05.00 Outside main frame, overview
LT-USAFA-1.02.05.10 Outside charge tube, carriage
LT-USAFA-1.02.02.01 Charge tube, tube segment
LT-USAFA-1.02.02.06 Charge tube, inside section
LT-USAFA-1.02.02.04 Charge tube, flange
LT-USAFA-1.02.02.09 Charge tube, measurement ring
LT-USAFA-1.06.02.00 Inside frame, overview
LT-USAFA-1.06.03.00 Carriage, test section
LT-USAFA-1.05.01.00 Fast acting valve, overview
LT-USAFA-1.05.04.00 Nozzle, expansion part
LT-USAFA-1.04.02.00 Test section, overview
LT-USAFA-1.04.02.00 Test section, sectional view
LT-USAFA-1.04.04.00 Probe chamber, overview
LT-USAFA-1.04.06.00 Model support, x-moveable
LT-USAFA-1.04.09.00 Model support, angle of attack
LT-USAFA-1.04.03.00 Diffuser section, overview
LT-USAFA-1.03.02.00 Vacuum tank, overview
LT-USAFA-1.03.07.01 Vacuum blind flange, ports
LT-USAFA-1.03.06.01 Security valve, overpressure valve
LT-USAFA-1.03.03.00 Roller guides, vacuum sealing
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