Sanctions Finder
Sanctions Finder
Good

Last Updated: April 20, 2026

c. Thrust vector control sub-systems, usable in “missiles”. Technical Note: Examples of methods of achieving thrust vector control specified in 9A108.c. are: 1. Flexible nozzle; 2. Fluid or secondary gas injection; 3. Movable engine or nozzle; 4. Deflection of exhaust gas stream (jet vanes or probes); or 5. Thrust tabs.

Code

9A108

EU Code

M2A1e

Category

ANNEX III - CATEGORY 9 — AEROSPACE AND PROPULSION

Subcategory

9A - Systems, Equipment and Components

Prohibited Supply To
IR
Authority
EU
Document

EU Regulation No 267/2012

Notes
  • Thrust vector control subsystems, usable in the systems specified in 1.A., except as provided in the Note below 2.A.1. for those designed for rocket systems that do not exceed the “range”/“payload” capability of systems specified in 1.A.;Technical Note:2.A.1.e. includes the following methods of achieving thrust vector control:a.Flexible nozzle;b.Fluid or secondary gas injection;c.Movable engine or nozzle;d.Deflection of exhaust gas stream (jet vanes or probes);e.Use of thrust tabs.
  • Rocket motor cases, ‘insulation’ components and nozzles therefor, usable in the systems specified in 1.A. or 19.A.1.
  • Technical Note:In 3.A.3. ‘insulation’ intended to be applied to the components of a rocket motor, i.e. the case, nozzle inlets, case closures, includes cured or semi-cured compounded rubber components comprising sheet stock containing an insulating or refractory material. It may also be incorporated as stress relief boots or flaps.Note:Refer to 3.C.2. for ‘insulation’ material in bulk or sheet form.
Program information
Program information

Have feedback, suggestions or need help navigating sanctions? Let's talk.

Let's discuss how Sanctions Finder can support you or your business or organization.