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US3932241A Expired / Lapsed US ⏱️ 0.0 years remaining

Propellants based on bis[N-(trinitroethyl)nitramino]ethane

Assignee: United States Department of the Army
•
Filing: 1970-07-06
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Granted: 1976-01-13
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Expires: 1990-07-06
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Abstract

Abstract Propellant compositions using bis[N-(trinitroethyl)nitramino]ethane as an oxidizer for smokeless propellants that additionally contain binder ingredients, crosslinking agent and other additives as desired.

Inventors

  • 👤 David C. Sayles

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-02 16:25
CPC Classifications
C; C06; C06B; C06B25/00; C06B25/36; C06B45/00; C06B45/04; C06B45/06; C06B45/10

Claims Analysis

Total Claims: 11
Claim 1
Independent Claim 38 words
A propellant composition comprising; an oxidizer including bis[N-(trinitroethyl)nitramino]ethane, an acrylate-acrylic acid binder, and a curing agent, said acrylate-acrylic acid being present in a ratio of acrylate to acrylic acid in an amount of about 90/10 to about 96/4.
Claim 2
Dependent Claim 38 words
A propellant composition comprising; an oxidizer including bis[N-(trinitroethyl)nitramino]ethane, an acrylate-acrylic acid binder, and a curing agent, said acrylate-acrylic acid being present in a ratio of acrylate to acrylic acid in an amount of about 90/10 to about 96/4.
Claim 3
Dependent Claim 13 words
The propellant composition of claim 1, wherein said oxidizer also includes ammonium perchlorate.
Claim 4
Dependent Claim 23 words
The propellant composition of claim 1, wherein said curing agent is diepoxy dicyclohexyl carboxylate, and said propellant composition further comprises a plasticizer, 1,2,3-tris[1,2-bis(difluoroamino)ethoxy]propane.
Claim 5
Dependent Claim 29 words
The propellant composition of claim 1, wherein said binder consists of a copolymer of acrylate-acrylic acid in an amount up to about 25 weight percent of the propellant composition.
Claim 6
Dependent Claim 37 words
The propellant composition of claim 1, wherein said curing agent is diepoxy dicyclohexyl carboxylate, and said propellant composition further comprises a plasticizer, 1,2,3-tris[1,2-bis(difluoroamino)ethoxy]propane, said binder to plasticizer being present in a ratio of about 1 to 5.
Claim 7
Dependent Claim 40 words
The propellant composition of claim 5, wherein said plasticizer and binder constitute from about 25 to about 35 weight percent of the propellant composition, and said oxidizer constitutes from about 65 to about 75 weight percent of said propellant composition.
Claim 8
Dependent Claim 14 words
The propellant composition of claim 6, wherein said acrylate-acrylic acid is ethyl acrylate-acrylic acid.
Claim 9
Dependent Claim 93 words
The propellant composition of claim 1, wherein said oxidizer consists of ammonium perchlorate of about 19.2 weight percent of the propellant composition and bis[N-(trinitroethyl)nitramino]ethane of about 48.6 weight percent of the propellant composition, said curing agent consists of diepoxy dicyclohexyl carboxylate of about 1.4 weight present of the propellant composition, and the propellant composition contains the additional ingredients carbon black in an amount of about 0.5 weight percent of the propellant composition, and a plasticizer, 1,2,3-tris[1,2-bis(difluoroamino)ethoxy]propane, of about 25.7 weight percent of the propellant composition, the remainder of said propellant composition being binder.
Claim 10
Dependent Claim 77 words
The propellant composition of claim 1, wherein said oxidizer consists of said bis[N-(trinitroethyl)nitramino]ethane in an amount of about 67.8 weight percent of the propellant composition, said curing agent is diepoxy dicyclohexyl carboxylate of about 1.4 weight percent of the propellant composition, and said propellant also contains carbon black in an amount of about 0.5 weight percent and a plasticizer, 1,2,3-tris[1,2-bis(difluoroamino)ethoxy]propane, of about 25.7 weight percent of the propellant composition, the remainder of said propellant composition being binder.
Claim 11
Dependent Claim 22 words
The propellant composition of claim 1, wherein said bis[N-(trinitroethyl)nitramino]ethane constitutes from about 50 to about 75 weight percent of the propellant composition.

References Cited (Backward Citations)

US2481283A Cited
US3038009A Cited
US3117044A Cited
US3389026A Cited
US3255059A Cited
US3476622A Cited
US3586552A Cited
US3804683A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1979-01-12 1979-07-14 1980-01-13 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1983-01-12 1983-07-14 1984-01-13 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1987-01-12 1987-07-14 1988-01-13 $7700.00 Window Closed / Lapsed

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