Flight control apparatus for an anti-tank projectile

Details Flight control apparatus for an anti-tank projectile Flight control apparatus for an anti-tank projectile

1990-09-28

1992-05-12

Jordan, Charles T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

244 328, F42B 1066

Patent

active

051115530

ABSTRACT:
Flight control apparatus (10) for a cannon-launched anti-tank projectile. A boom that structurally secures four fins (18) and four nozzles (20) to an afterbody (12) of the projectile, and that provides for fluid communication from the afterbody to the nozzles, is provided in the form of an assembly (14) comprising intersecured tubes (22, 24, 26, 28) which define a longitudinal axis (30) of the assembly. The boom assembly (14) considerably reduces the weight and fabrication cost associated with a conventional boom which is provided in the form of an integral multi-channeled cylinder.

REFERENCES:
patent: 3390850 (1968-07-01), Dahlke et al.

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