Patent US4209351A successfully refreshed from Google Patents.
← Back to Patent Explorer
US4209351A Expired / Lapsed US ⏱️ 0.0 years remaining

Ambient cured smokeless liner/inhibitor for propellants

Assignee: United States Department of the Army
•
Filing: 1978-06-05
•
Granted: 1980-06-24
•
Expires: 1998-06-05
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract A liner composition is employed as a liner/inhibitor for a solid propellant grain while functioning as a liner-binder between the propellant grain and insulation or the motor case. The liner and inhibitor composition is prepared from the conventional binder systems (e.g., hydroxy terminated polybutadiene (HTPB), polysulfide, polyurethane, and polyester). The composition employs a cool burning oxidizer selected from oxamide and nitroguanidine. The type of solid propellant grain, particularly the crosslinking or reaction mechanism to form a chemical bond between the binder of the liner composition and the binder of the propellant, dictates the type formulation of the liner/inhibitor composition. A representative liner/inhibitor for a HTPB propellant grain contains from about 10 to about 70 weight percent oxidizer, from about 0.1 to about 1.0 weight percent cure catalyst selected from ferric acetyl acetonate and triphenyl bismuth, an isocyanate curing agent selected from toluene diisocyanate, hexamethylene diisocyanate, and isophorone diisocyanate from about 1 to about 10 weight percent, and the balance of formulation hydroxy terminated polybutadiene. The use of the proper cure catalyst will produce a cured system at ambient (70 DEG F. or higher) in 24 hours. A chemical bond is formed between the liner and inhibitor binder and the propellant binder by the crosslinking action of the isocyanate curing agent and the hydroxyl groups of the binder systems. The chemical bond withstands the stresses of gas flow as well as the effects of spinning the rocket motor. Thus, the cool burning oxidizer in combination with the bonds between the binder systems which withstands the flow of gases will result in extinguishment of the liner/inhibitors at sudden pressure drop encountered at end of propellant grain burning and thereby result in elimination of smoke from the liner/inhibitor which is extinguished prior to bond failure.

Inventors

  • 👤 Everette M. Pierce
  • 👤 Henry C. Allen

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-28 10:27
CPC Classifications
F; F02; F02K; F02K9/00; F02K9/08; F02K9/32; F02K9/34; F02K9/346

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 189 words
An ambient cured smokeless liner/inhibitor composition for use with a solid propellant grain to establish a chemical bond between said liner/inhibitor binder and the binder system of said solid propellant grain, said solid propellant binder system selected from the group consisting of hydroxy terminated polybutadiene, polysulfide, polyurethane, and polyester, said smokeless liner/inhibitor composition comprising: (i) a liner/inhibitor binder of polysulfide in an amount from about 19.0 to about 70.0 weight percent of said liner/inhibitor composition; (ii) a curing agent selected from the group consisting of lead peroxide, cumene hydroperoxide, zinc oxide, p-quinone dioxime, zinc peroxide, toluene diisocyanate, hexamethylene diisocyanate, and isophorone diiscyanate in an amount from about 1.0 to about 10.0 weight percent of said liner/inhibitor composition; (iii) a cure catalyst selected from the members of the goup of catalysts consisting of inorganic cobalt salts, furfural, chromium octoate, ferric acetyl acetonate and triphenyl bismuth in an amount from about 0.1 to about 1.0 weight percent of said liner/inhibitor composition; and (iv) a cool burning oxidizer selected from the group consisting of oxamide and nitroguanidine in an amount from about 10.0 to about 70.0 weight percent of said liner/inhibitor composition.
Claim 2
Dependent Claim 189 words
An ambient cured smokeless liner/inhibitor composition for use with a solid propellant grain to establish a chemical bond between said liner/inhibitor binder and the binder system of said solid propellant grain, said solid propellant binder system selected from the group consisting of hydroxy terminated polybutadiene, polysulfide, polyurethane, and polyester, said smokeless liner/inhibitor composition comprising: (i) a liner/inhibitor binder of polysulfide in an amount from about 19.0 to about 70.0 weight percent of said liner/inhibitor composition; (ii) a curing agent selected from the group consisting of lead peroxide, cumene hydroperoxide, zinc oxide, p-quinone dioxime, zinc peroxide, toluene diisocyanate, hexamethylene diisocyanate, and isophorone diiscyanate in an amount from about 1.0 to about 10.0 weight percent of said liner/inhibitor composition; (iii) a cure catalyst selected from the members of the goup of catalysts consisting of inorganic cobalt salts, furfural, chromium octoate, ferric acetyl acetonate and triphenyl bismuth in an amount from about 0.1 to about 1.0 weight percent of said liner/inhibitor composition; and (iv) a cool burning oxidizer selected from the group consisting of oxamide and nitroguanidine in an amount from about 10.0 to about 70.0 weight percent of said liner/inhibitor composition.
Claim 3
Dependent Claim 77 words
The ambient cured smokeless liner/inhibitor composition of claim 1 wherein said liner/inhibitor binder selected is polysulfide in an amount of about 46 weight percent of said liner/inhibitor composition; said curing agent selected is isophorone diisocyanate in an amount of about 6.3 weight percent of said liner/inhibitor composition; said cure catalyst selected is chromium octoate in an amount of about 0.4 weight percent; and said cool burning oxidizer selected is oxamide in amount of about 47.3 weight percent.
Claim 4
Dependent Claim 22 words
The ambient cured smokeless liner/inhibitor composition of claim 2 wherein said solid propellant grain employs the selected propellant binder system of polysulfide.
Claim 5
Dependent Claim 24 words
The ambient cured smokeless liner/inhibitor composition of claim 2 wherein said solid propellant grain employs the selected propellant binder system of hydroxy terminated polybutadiene.

References Cited (Backward Citations)

US2997376A Cited
US3046829A Cited
US3706610A Cited
US3278352A Cited
US3433158A Cited
US3636881A Cited
US3507114A Cited
US3714047A Cited
US3726829A Cited
US4111728A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1983-06-24 1983-12-24 1984-06-24 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1987-06-24 1987-12-24 1988-06-24 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1991-06-24 1991-12-24 1992-06-24 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag