Patents Represented by Attorney Sciascia R.

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  • Method of controlling the spin rate of tube launched rockets
    Patent number: 3964696
    Abstract: The spin rate of a rocket missile is controlled by bevelling the inside of he leading edge of the missile fins. Altering the bevel angle controls the rate of spin. The spin rate is also controlled by sweeping back the leading edges of the fins.
    Type: Grant
    Filed: October 30, 1974
    Date of Patent: June 22, 1976
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Casimir T. Orzechowski, Nat Seiden, Anthony Mycka, Jr.