Patent US4458482A successfully refreshed from Google Patents.
← Back to Patent Explorer
US4458482A Expired / Lapsed US ⏱️ 0.0 years remaining

Rocket motor

Assignee: United States Department of the Navy
•
Filing: 1982-05-17
•
Granted: 1984-07-10
•
Expires: 2002-05-17
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract A bare patch in an insulating coating on a cylinder is shaped to reinforcetress patterns to cause failure at a predetermined point as a cook-off safety feature.

Inventors

  • 👤 Ronald F. Vetter
  • 👤 Theodore A. Hicks
  • 👤 Warren R. Compton

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-31 09:05
CPC Classifications
F; F02; F02K; F02K9/00; F02K9/08; F02K9/32; F02K9/38; F42; F42B; F42B39/00; F42B39/20

Claims Analysis

Total Claims: 10
Claim 1
Independent Claim 77 words
A rocket motor having a reduced likelihood of explosion in an external fire, comprising: a cylindrical casing; propellant grain, having a central void, contained within said casing; coating means applied to selected exterior areas of said casing to protect said rocket motor casing from an external fire; and a bare portion in said coating means, said bare portion having a shape to intensify heat produced stress in a predetermined area to cause failure at a predetermined point.
Claim 2
Dependent Claim 77 words
A rocket motor having a reduced likelihood of explosion in an external fire, comprising: a cylindrical casing; propellant grain, having a central void, contained within said casing; coating means applied to selected exterior areas of said casing to protect said rocket motor casing from an external fire; and a bare portion in said coating means, said bare portion having a shape to intensify heat produced stress in a predetermined area to cause failure at a predetermined point.
Claim 3
Dependent Claim 14 words
A rocket motor according to claim 1 wherein said coating means includes: insulating paint.
Claim 4
Dependent Claim 15 words
A rocket motor according to claim 1 wherein said bare portion is of cruciform shape.
Claim 5
Dependent Claim 15 words
A rocket motor according to claim 1 wherein said bare portion is of oval shape.
Claim 6
Dependent Claim 15 words
A rocket motor according in claim 1 wherein said bare portion is of triangular shape.
Claim 7
Dependent Claim 24 words
A rocket motor according to claim 3 wherein the intersection of said cruciform are at a predetermined location with respect to said center void.
Claim 8
Dependent Claim 24 words
A rocket motor according to claim 4 wherein the axis of said oval are at a predetermined location with respect to said center void.
Claim 9
Dependent Claim 109 words
A rocket motor comprising: a cylindrical casing; a propellant grain contained within said casing said propellant grain including, a central, axially extending void, and a plurality of radial slots extending from said central void toward said casing; a heat insulating coating covering substantially all of the exterior of said casing; and a bare spot of predetermined shape extending through said heat insulating coating to expose said casing having a center located between adjacent ones of said radial slots, whereby heat generated stress causes casing failure near said center to delay ignition along said central void or radial slots by relieving internal pressure and causing venting through said casing failure.
Claim 10
Dependent Claim 109 words
A rocket motor comprising: a cylindrical casing; a propellant grain contained within said casing said propellant grain including, a central, axially extending void, and a plurality of radial slots extending from said central void toward said casing; a heat insulating coating covering substantially all of the exterior of said casing; and a bare spot of predetermined shape extending through said heat insulating coating to expose said casing having a center located between adjacent ones of said radial slots, whereby heat generated stress causes casing failure near said center to delay ignition along said central void or radial slots by relieving internal pressure and causing venting through said casing failure.

References Cited (Backward Citations)

US2917424A Cited
US3032975A Cited
US3188802A Cited
US3152548A Cited
US3130940A Cited
US3446018A Cited
US3426528A Cited
US3583162A Cited
US3713395A Cited
US3946557A Cited
US3992997A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1987-07-10 1988-01-09 1988-07-10 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1991-07-10 1992-01-09 1992-07-10 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1995-07-10 1996-01-09 1996-07-10 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag