Abstract: 1. A slot former assembly for use in fabricating the solid propellant in a motor case for a solid propellant rocket motor comprising an outer hollow core, an inner tubular core and a flexible slot former comprising a skeleton frame consisting of stiffening rods that are retained in spaced relation to each other by means of a cord woven thereon in a basket weave and provided with a covering of flexible material operatively connected to said hollow core, whereby when said assembly is positioned in said motor case and the solid propellant is cast therein about said assembly, a slotted cavity configuration will be provided in the solid propellant in said motor case.

Abstract: Stresses induced by differential expansion and contraction of the solid propellant grain and the rocket motor case to which it is conventionally bonded are obviated by bonding a special sheath to the propellant grain and attaching it to the rocket motor case only at its forward and aft ends. A thin layer of Teflon is confined intermediately between the sheath and the rocket motor case. The sheath is extended beyond the propellant grain and bonded to the case so that an unbonded section thereof extends between the zone at which it is bonded to the case and the propellant grain. The propellant grain joins the sheath by a surface fillet to relieve surface stresses at this juncture. A gastight seal is provided in the thrust nozzle of the rocket motor for pressurizing of the combustion chamber to inhibit radial shrinkage of the propellant.

Abstract: The forward end of a rocket motor is attached, by a threaded adapter, to a cylindrical housing that is in turn attached to an elongated tube, the opposite end of which is fitted with a releasable nose cone. The elongated tube is filled with a series of bombs. Each bomb is a conical, shaped charge equipped at one end with a parachute protected by a split, conical, plastic shield loosely held together by a band and a pronged clip--all of which is seated in the conical recess of an adjacent bomb. A conical partition separates the tube from the housing; and the main parachute is attached in the housing. An acceleration actuated fuse in the adapter ignites a time delay charge, which ignites an explosive charge that when exploded forces a piston against the housing, so that it separates the housing and tube from the adapter and rocket.

Abstract: An improved projectile suitable for use in artillery pieces, though preferably in the higher calibres, is disclosed wherein projectile range upon launching by the gun is considerably extended by means of a propellant rocket motor in combination therewith which motor is characterized by containing in its combustion chamber a flowable propellant charge in the form of a fluidizable, shapeable propellant charge composition which under the high radial acceleration forces imparted to the projectile when fired from a rifled gun barrel, flows and shapes itself into the shape of a hollow cylinder and, when ignited in flight, burns in the manner of a solid propellant grain of the same shape to aid in propelling the projectile a greater distance than is possible with the gun alone.