OFFICIAL NOTICE

This project and all associated technical documentation have been withdrawn from public display at the request of the relevant Federal Agency (name withheld).

All materials related to guided missile systems, including but not limited to:

• Propulsion system integration with guidance and control systems
• Fin-stabilization and active control mechanisms
• Targeting and navigation subsystems
• Weaponization applications and dual-use technologies
• Technical specifications, CAD models, and design documentation

have been removed from this website and are no longer accessible to the public.

This action was taken in accordance with federal regulations governing dual-use technologies and national security considerations under the International Traffic in Arms Regulations (ITAR) and Export Administration Regulations (EAR).

The withdrawal is effective immediately and applies to all digital and physical copies of project materials previously made available through this platform.