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US4707199A Expired / Lapsed US ⏱️ 0.0 years remaining

Non nitroglycerin-containing composite-modified double-base propellant

Assignee: United States Department of the Army
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Filing: 1983-10-17
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Granted: 1987-11-17
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Expires: 2003-10-17
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Abstract

Abstract The glycidyl azide polymer produced by hydrolysis of glycidyl chloride followed by reaction with sodium azide is employed in a crosslinked composite-modified double-base propellant composition both in the casting powder portion and casting solvent portion as a superior replacement for nitroglycerin in each portion specified. The crosslinked composite-modified double-base propellant composition is characterized by having a greater safety in handling, reduced sensitivity to detonation, higher burning rate, higher specific impulse, and improved mechanical properties as compared with a like composition containing nitroglycerin in the casting powder and the casting solvent portions.

Inventors

  • 👤 David C. Sayles

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-31 09:24
CPC Classifications
C; C06; C06B; C06B45/00; C06B45/04; C06B45/06; C06B45/10; C06B45/105

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 184 words
A crosslinked composite-modified double-base propellant composition comprising a casting powder portion and a casting solvent portion, said casting powder portion comprising about 72.0 weight percent of said propellant composition and said casting solvent portion comprising about 28.0 weight percent of said propellant composition, said casting powder portion comprised in part by weight of ingredients as follows: ______________________________________ nitrocellulose (12.5% nitrogen) 16.6 carboranylmethyl propionate 4.7 triacetin 17.5 2-nitrodiphenylamine 1.1 resorcinol 0.7 ammonium perchlorate (1 μm) 32.8 aluminum (20 μm) 7.2 aluminum staple (whiskers) 2.7 glycidyl azide polymer formed from hydrolysis 16.0 of glycidyl chloride followed by reaction with sodium azide ______________________________________ , and said casting solvent portion comprised in parts by weight of ingredients as follows: ______________________________________ glycidyl azide 45.8 triacetin 52.7 hexane diisocyanate 0.50 triphenylbismuthine 0.07 ______________________________________ , said crosslinked composite-modified double-base propellant composition characterized by having greater safety in handling, reduced sensitivity to detonation, higher burning rate, higher specific impulse, and improved mechanical properties as compared with a like composition containing nitroglycerin in said casting powder portion and in said casting solvent portion in equivalent molar weight amounts to said glycidyl azide polymer.
Claim 2
Dependent Claim 184 words
A crosslinked composite-modified double-base propellant composition comprising a casting powder portion and a casting solvent portion, said casting powder portion comprising about 72.0 weight percent of said propellant composition and said casting solvent portion comprising about 28.0 weight percent of said propellant composition, said casting powder portion comprised in part by weight of ingredients as follows: ______________________________________ nitrocellulose (12.5% nitrogen) 16.6 carboranylmethyl propionate 4.7 triacetin 17.5 2-nitrodiphenylamine 1.1 resorcinol 0.7 ammonium perchlorate (1 μm) 32.8 aluminum (20 μm) 7.2 aluminum staple (whiskers) 2.7 glycidyl azide polymer formed from hydrolysis 16.0 of glycidyl chloride followed by reaction with sodium azide ______________________________________ , and said casting solvent portion comprised in parts by weight of ingredients as follows: ______________________________________ glycidyl azide 45.8 triacetin 52.7 hexane diisocyanate 0.50 triphenylbismuthine 0.07 ______________________________________ , said crosslinked composite-modified double-base propellant composition characterized by having greater safety in handling, reduced sensitivity to detonation, higher burning rate, higher specific impulse, and improved mechanical properties as compared with a like composition containing nitroglycerin in said casting powder portion and in said casting solvent portion in equivalent molar weight amounts to said glycidyl azide polymer.

References Cited (Backward Citations)

US4288262A Cited
US4269637A Cited
US4379894A Cited
US4379903A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1990-11-16 1991-05-18 1991-11-17 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1994-11-16 1995-05-18 1995-11-17 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1998-11-16 1999-05-18 1999-11-17 $7700.00 Window Closed / Lapsed

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