Solid fuel rocket projectile - has radial burner propellant support tube which serves as carrier for ignition charge

摘要

The tubular support (10) is intended for a solid propellant unit (12) of a radial burner, partic. for a rocket projectile, and has an enclosed wall (11). The tubular support serves as a carrier for the ignition charge (17). The tube wall may be provided with recesses. The ignition charge may be arranged on at least one surface of the tube, in recesses. The tube wall may have ignition orifices (18). A further tube with ignition orifices may be co-axially arranged around the support tube. The charge may be arranged in the orifices of the support tube.