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US4062709A Expired / Lapsed US ⏱️ 0.0 years remaining

Inhibited fluorocarbon rocket propellant

Assignee: Individual
•
Filing: 1968-09-25
•
Granted: 1977-12-13
•
Expires: 1988-09-25
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Abstract

Abstract A fluorocarbon bound rocket propellant grain provided with a compatible burn inhibitor on selected areas, particularly the outer surface, which is inexpensive and simple to apply.

Inventors

  • 👤 Victor F. Castaneda
  • 👤 Homer L. Davis

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-03 18:34
CPC Classifications
C; C06; C06B; C06B45/00; C06B45/12; C06B21/00; C06B21/0083

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 74 words
The method of restricting the burning of fluorocarbon bound propellant grains which comprises spraying the grain with a mixture consisting of 80 parts by weight modified diglycidyl ether of para, para'-isopropylidenediphenol, and 20 parts by weight polymeric amido-amine hardner at a temperature ranging from 100° F. to 150° F., permitting a layer of said mixture to deposit on said grain, and cooling for about one hour at room temperature until said layer is cured.
Claim 2
Independent Claim 74 words
The method of restricting the burning of fluorocarbon bound propellant grains which comprises spraying the grain with a mixture consisting of 80 parts by weight modified diglycidyl ether of para, para'-isopropylidenediphenol, and 20 parts by weight polymeric amido-amine hardner at a temperature ranging from 100° F. to 150° F., permitting a layer of said mixture to deposit on said grain, and cooling for about one hour at room temperature until said layer is cured.
Claim 3
Dependent Claim 46 words
The method of claim 1 wherein said propellant consists essentially of about 15% by weight polytetrafluoroethylene, about 15% by weight of the copolymer of vinylidene fluoride and perfluoropropylene, about 49.5% by weight ammonium perchlorate, about 19.5% by weight aluminum and about 1% by weight sodium fluoride.
Claim 4
Dependent Claim 87 words
The fluorocarbon bound propellant grain having its outer surface covered with a layer of restrictive burning material consisting essentially of a mixture of about 80 parts by weight modified diglycidyl ether of para, para'-isopropylidenediphenol type liquid epoxy resin and about 20 parts by weight of a polymeric amido-amine hardner; said grain comprising about 15% by weight polytetrafluoroethylene, about 15% by weight of the copolymer of vinylidene fluoride and perfluoropropylene, about 49.5% by weight ammonium perchlorate, about 19.5% by weight aluminum and about 1% by weight sodium fluoride.
Claim 5
Dependent Claim 87 words
The fluorocarbon bound propellant grain having its outer surface covered with a layer of restrictive burning material consisting essentially of a mixture of about 80 parts by weight modified diglycidyl ether of para, para'-isopropylidenediphenol type liquid epoxy resin and about 20 parts by weight of a polymeric amido-amine hardner; said grain comprising about 15% by weight polytetrafluoroethylene, about 15% by weight of the copolymer of vinylidene fluoride and perfluoropropylene, about 49.5% by weight ammonium perchlorate, about 19.5% by weight aluminum and about 1% by weight sodium fluoride.

References Cited (Backward Citations)

US2977884A Cited
US2987388A Cited
US2999462A Cited
US3012508A Cited
US3012506A Cited
US3012507A Cited
US2917424A Cited
US2976678A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1980-12-12 1981-06-13 1981-12-13 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1984-12-12 1985-06-13 1985-12-13 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1988-12-12 1989-06-13 1989-12-13 $7700.00 Window Closed / Lapsed

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