RAKETENVERKLEIDUNG MIT HÜLSE, DIE EINE RADIALE UND/ODER AXIALE LOCKERUNG AUFWEIST

摘要

The rocket cap (14) comprises an ogival shell (20) made of a first material and a ferrule (22) made of a second material for fixing the ogival shell (20) to a rocket body. The ferrule (22) comprises a sleeve (32) centered on an axis (A-A '), fitted with the ogival shell (20) and glued to the ogival shell (20). This sleeve (32) has a radial softening able to absorb the radial thermal expansion of the sleeve (32), and / or an axial softening able to absorb the axial thermal expansion of the sleeve (32).