Abstract: The conventional monocoque missile ordnance section is replaced by a compte sheet stringer design. The composite sheet stringer design consists of a full-length, filamentary composite outer shell attached to stringers. Bending and axial loads are carried by the stringers while the outer shell will resist shear loads. The forward part of the ordnance section is devoted to the warhead. Here, fragment material would be sandwiched between the stringers, the outer shell, and possibly a filamentary composite inner shell. Fragment options include discrete fragments, plates, or rods. The aft part of the ordnance section would be available for fuzing assemblies. The composite ordnance section is connected to the rest of the missile through end joints rigidly attached to the outer composite shell and stringers.

Abstract: A method of guiding an in-flight vehicle toward a target exhibiting a known or predictable thrusting profile is provided. The vehicle undergoes an alternating series of vehicle coasts and diverts during the vehicle's terminal intercept phase of flight. Position and velocity information of the target with respect to the vehicle is used to select a course change during each vehicle coast. The course change is intentionally offset from a collision course with the target and is effected by the next divert in the series. The amount of offset is such that the final coast results in a target intercept.