Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage
Patent
1992-07-10
1993-12-21
Tudor, Harold J.
Aeronautics and astronautics
Missile stabilization or trajectory control
Externally mounted stabilizing appendage
102348, 244 90R, 244 326, 273416, 446 66, F42B 1012
Patent
active
052715795
ABSTRACT:
A recreational rocket (10) has a nose cone assembly (18,33) movable with respect to the main rocket body 12 between two limits. Each of a pair of fins (20) on the nose cone assembly (18,33) has a hinged aileron (22). The ailerons (22) are held in a straight path course by a limit bar (37) on body (12) when the nose cone assembly is at one limit. Plastic members (42) pull the ailerons (22) into glide mode position against the edges of stanchion plates (38).
REFERENCES:
patent: Re26882 (1970-05-01), Turner
patent: 2876585 (1959-03-01), Zaic
patent: 3091889 (1963-06-01), Zaic
patent: 3888178 (1975-06-01), Senoski
patent: 3903801 (1975-09-01), Senoski
patent: 3942441 (1976-03-01), Senoski
patent: 5139215 (1992-08-01), Peckham
Netter George J.
Tudor Harold J.
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