Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage
Patent
1980-02-01
1982-04-06
Tudor, Harold J.
Aeronautics and astronautics
Missile stabilization or trajectory control
Externally mounted stabilizing appendage
244 329, F42B 1332, F42B 1516
Patent
active
043232086
ABSTRACT:
A folding fin assembly (2) for a flight vehicle in which a fin (3) is carried for rotation about a chordwise axis (Z--Z) upon a turntable (9), the turntable (9) being itself turnable with reference to a fixed base (5) about a given axis (W--W) transverse to the chordwise axis (Z--Z). This is effected by meshing worm gears (14, 8) which transmit rotary movement to the turntable (9) as the fin (3) is rotated about the chordwise axis. The fin (3) lies flat against the surface of the flight vehicle with its chordwise axis (Z--Z) transverse to a fore-and-aft axis (X--X) of the flight vehicle and on erection is turned so that the chordwise axis (Z--Z) lies parallel to the fore-and-aft axis (X--X) of the flight vehicle.
REFERENCES:
patent: 3023854 (1962-03-01), Lohr
patent: 3063375 (1962-11-01), Hawley et al.
patent: 3098445 (1963-07-01), Jackson
British Aerospace
Tudor Harold J.
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