(under the class definition) Apparatus and corresponding methods wherein an aerial missile or payload carrying or containing a propelling charge which charge when ignited
generates gases which are directed radially and axially or omni-directionally from the longitudinal axis of the missile.
(1) Note. The subject matter is peculiarly adapted for use with a relatively stationary launching structure, such as a gun barrel or cartridge case, to sufficiently enclose the propelling charge to provide an axial propulsion force between the missile and the relatively stationary launching structure.
