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US3964696A Expired / Lapsed US ⏱️ 0.0 years remaining

Method of controlling the spin rate of tube launched rockets

Assignee: United States Department of the Navy
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Filing: 1974-10-30
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Granted: 1976-06-22
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Expires: 1994-10-30
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Abstract

Abstract The spin rate of a rocket missile is controlled by bevelling the inside ofhe 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.

Inventors

  • 👤 Casimir T. Orzechowski
  • 👤 Nat Seiden
  • 👤 Anthony Mycka, Jr.

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-08 09:45
CPC Classifications
F; F42; F42B; F42B10/00; F42B10/02; F42B10/14; F42B10/16; F42B10/26; F42B10/28; F42B10/30

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 67 words
Means for improving the ballistic accuracy of a missile comprising: a set of fins located around the body of a missile, said fins being curved in the radial direction of the missile and being formed with a bevel along the concave side of the leading edge of the fin, the leading edge of said fin also being formed with a sweep-back angle along the entire leading edge.
Claim 2
Dependent Claim 67 words
Means for improving the ballistic accuracy of a missile comprising: a set of fins located around the body of a missile, said fins being curved in the radial direction of the missile and being formed with a bevel along the concave side of the leading edge of the fin, the leading edge of said fin also being formed with a sweep-back angle along the entire leading edge.
Claim 3
Dependent Claim 14 words
Means as set forth in claim 1, wherein the sweep-back angle is roughly 45°.
Claim 4
Dependent Claim 17 words
Means as in claim 1, wherein the bevel angle lies roughly in the 5° to 45° range.
Claim 5
Dependent Claim 12 words
Means as in claim 3, wherein the bevel angle is roughly 22°.

References Cited (Backward Citations)

US2145508A Cited
US3177809A Cited
US3333790A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1979-06-22 1979-12-22 1980-06-22 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1983-06-22 1983-12-22 1984-06-22 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1987-06-22 1987-12-22 1988-06-22 $7700.00 Window Closed / Lapsed

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