SATPC0038184 Tab 04 4 Specification Rev.pdf

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Attached to
Aerolab Educational Wind Tunnel (EWT) & Wind Tunnel Control Software Federal contract opportunity
Solicitation number
80NSSC25901316Q
Issued by
National Aeronautics and Space Administration Shared Services Center

About this file

This document is a specification sheet for a wind tunnel, detailing precise technical requirements for an educational wind tunnel system. The specifications mandate an open circuit design with a downstream fan and computer-controlled airspeed or fan RPM. The test section must measure 12" x 12" x 24" (with ±0.5" tolerance), support maximum flow velocities over 100 mph, and fit within overall dimensions of 6' x 6' x 16'. The system requires 480VAC three-phase power and must be deliverable within 26 weeks after receipt of order (ARO). These specifications align with NASA's solicitation for an Aerolab Educational Wind Tunnel (EWT) and Wind Tunnel Control Software, indicating a targeted procurement for specific research and educational equipment.

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SATPC0038184 Tab 07 Capability Statement Commercial.pdf PDF

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Text version

Wind Tunnel Specifications

• Must be open circuit design

• Must use a downstream fan

• Must include computer control of airspeed or fan RPM

Test section dimensions (H x W x L) 12” x 12” x 24” (± 0.5” all dimensions) Maximum test section flow velocity > 100 mph Maximum overall dimensions (H x W x L) 6’ x 6’ x 16’ Voltage 480VAC three phase

Lead time ARO < 26 weeks

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