This invention is a long thin rocket that launches forward and glides backward
after an ejection pitch maneuver with no moving parts. It takes advantage of a
shift in center of pressure caused by a change in the angle of incidence of the
rocket. This change in angle of incidence is caused by the side thrust pitch maneuver.
The pitch maneuver is initiated by the ejection charge out a side thrust port or
other side thrusting apparatus at a location on the rocket causing a large torque
about the center of gravity of the rocket. The center of gravity of the rocket
after the pitch is optimally less than 60% of the way between the Barrowman center
of pressure and the center of lateral area center of pressure.
