Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control
Patent
1975-12-02
1980-10-21
Tudor, Harold J.
Aeronautics and astronautics
Missile stabilization or trajectory control
Remote control
102 921, 244 33, F42B 1518, F42B 1510, F42B 1300
Patent
active
042289734
ABSTRACT:
An infantry projectile includes an elongated projectile body having a cylindrical or frusto-conical surface concentrically arranged about its longitudinal axis. The projectile body has a leading end and a trailing end each extending transversely of the longitudinal axis. The leading end is disposed at an oblique angle to the longitudinal axis for affording a trimming action on the projectile when it is in flight. A flow control projection is provided on the surface of the projectile body between its ends so that the aerodynamic center of the projectile is located below its center of gravity when the flow control projection is located on the lower surface of the projectile body and in a vertical plane extending through the longitudinal axis of the body.
REFERENCES:
patent: 2922365 (1960-01-01), Fredette et al.
patent: 3869101 (1975-03-01), Schnabele et al.
Messerschmitt-Bolkow-Blohm GmbH
Tudor Harold J.
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