Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1975-12-16
1990-07-17
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
244 324, F42B 1064
Patent
active
049416278
ABSTRACT:
A hollow fin of rhombical cross-section constructed of Nitinol or other memory effect alloy and mounted for oscillation about an internal shaft. The memory effect alloy has been previously stretched at a temperature below its critical transition temperature whereby heating of one pair of opposite sides, in a rhombic sense, above the critical transition temperature by resistive dissipation of an electric current will cause shortening of this pair of sides and consequent change in the angle of attack.
REFERENCES:
patent: 3153203 (1964-06-01), Halsted
patent: 3403238 (1968-09-01), Buchler et al.
Jackson, C. M. et al., "55-Nitinol--The Alloy With a Memory: Its Physical tallurgy, Properties, and Applications." NASA-SP 5110, 1972.
Jordan Charles T.
Lewis John D.
The United States of America as represented by the Secretary of
Walden Kenneth E.
Wendtland Richard W.
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