Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage
Patent
1990-06-01
1991-04-02
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Externally mounted stabilizing appendage
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
Hans Paul C.
Rosenfield Gary C.
Aerotech, Inc.
Jordan Charles T.
Mybeck Richard R.
Wendtland Richard W.
LandOfFree
Finlock alignment mechanism for rockets does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Finlock alignment mechanism for rockets, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Finlock alignment mechanism for rockets will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-323212