Pivoting guidance mechanism for small-calibered projectiles

Details Pivoting guidance mechanism for small-calibered projectiles Pivoting guidance mechanism for small-calibered projectiles

1984-07-25

1986-07-15

Kyle, Deborah L.

Aeronautics and astronautics

Missile stabilization or trajectory control

Externally mounted stabilizing appendage

244326, 102385, F42B 1332

Patent

active

046001670

ABSTRACT:
A pivoting guidance mechanism for small-calibered projectiles, missiles or small bombs with fins, which are form-fittingly fixed and axially oriented within a housing, are pivotable transverse to the longitudinal axis and guided in longitudinal slots in the housing, and which include a slider for extending the fins which is actuatable through a pretensioned, central coil spring.

REFERENCES:
patent: 3819132 (1974-06-01), Rusbach
patent: 3921937 (1975-11-01), Voss et al.

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