Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage
Patent
1989-12-18
1990-12-18
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Externally mounted stabilizing appendage
102529, F42B 1320, F42B 1332, F42B 1316
Patent
active
049780883
ABSTRACT:
A guidance mechanism for a subcaliber-sized fin-stabilized practice projectile including wings or vanes which are radially fixedly arranged on the shank of the projectile. The wings or vanes possess auxiliary vanes which extend transversely of their main axes, and wherein a hole which is produced in a target board by the fin-stabilized practice projectile corresponds, in general, with the diameter of a circle about which the auxiliary vanes are located on the projectile.
REFERENCES:
patent: 3015269 (1962-01-01), Potts, Jr.
patent: 3684214 (1972-08-01), Kloss
patent: 3845922 (1974-11-01), Mayer
patent: 4736909 (1988-04-01), Boder et al.
patent: 4815682 (1989-03-01), Feldmann et al.
Bock Erich
Brand Heinrich
Dommer Josef
Himmert Rainer
Carone Michael J.
Diehl GmbH & Co.
Jordan Charles T.
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