Finlock alignment mechanism for rockets

Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage

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244 33, F42B 1006

Patent

active

050041860

ABSTRACT:
A finlock mechanism for recreational rockets having a pair of finlock ring members disposed in spaced relationship to each other in circumscription about the motor tube in the rocket, each ring member having a plurality of finlock receptors disposed on the perimeter thereof in equispaced relationship to each other for receiving a finlock root extending through the rocket housing in snaplock engagement therewithin.

REFERENCES:
patent: 2691495 (1954-10-01), Chiroky
patent: 2842058 (1958-07-01), Kuller et al.
patent: 2851950 (1958-09-01), Van Aken et al.
patent: 3032857 (1962-05-01), Lyon
patent: 3117520 (1964-01-01), Kerr et al.
patent: 3158100 (1964-11-01), Finley
patent: 3687398 (1972-08-01), Beuschel

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