ECCN.DEV by Cancelli

9B105 Category 9B

‘Aerodynamic test facilities’ for speeds of Mach 0.9 or more, usable for rockets, missiles, or unmanned aerial vehicles capable of achieving a “range” equal to or greater than 300 km and their subsystems.

Category 9: Aerospace and Propulsion

Reasons for control

Country chart

ControlColumn
AT applies to entire entryAT 1
MT applies to entire entryMT 1

List-based license exceptions

ExceptionAs stated in the entry
GBS N/A
LVS N/A

Items

  1. Items: The list of items controlled is contained in the ECCN heading.

Related controls

See also 9B005

Notes

Note: 9B105 does not control wind tunnels for speeds of Mach 3 or less with the dimension of the ‘test cross section size’ equal to or less than 250 mm.

Technical Notes: 1. ‘Aerodynamic test facilities’ includes wind tunnels and shock tunnels for the study of airflow over objects. 2. ‘Test cross section size’ means the diameter of the circle, or the side of the square, or the longest side of the rectangle, or the major axis of the ellipse at the largest ‘test cross section’ location. ‘Test cross section’ is the section perpendicular to the flow direction.

Source: eCFR, version 2026-08-01, retrieved 2026-08-20T04:04:59+00:00.