‘Interior lining’ usable for rocket motor cases in the systems specified in 1.A. or specially designed for systems specified in 19.A.1. or 19.A.2.

Items, materials, equipment, goods and technology related to ballistic missile programmes

CATEGORY II ITEM 3 - PROPULSION COMPONENTS AND EQUIPMENT

S/2012/947

Technical Note: In 3.C.1. ´interior lining´ suited for the bond interface between the solid propellant and the case or insulating liner is usually a liquid polymer based dispersion of refractory or insulating materials e.g. carbon filled HTPB or other polymer with added curing agents to be sprayed or screeded over a case interior.