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US4070213A Expired / Lapsed US ⏱️ 0.0 years remaining

Dispersing aids for MT-4

Assignee: United States Department of the Army
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Filing: 1976-06-30
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Granted: 1978-01-24
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Expires: 1996-06-30
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Abstract

Abstract Diols of the general formula, R(OH)2, wherein R is an alkylene radical, and iminodiols of the general formula, R'N(R''OH)2, wherein R' is an aryl or alkyl radical and R'' is an alkylene radical, with melting points of less than 60 DEG C (140 DEG F) are effective dispersing aids for the bonding agent MT-4. MT-4 which functions as an interfacial bonding agent is prepared by reacting together 2.0 moles of tris 1(2 methylaziridinyl)phosphine oxide, 0.7 mole adipic acid, and 0.3 mole tartaric acid. The specified dispersing aids react to become a part of the binder matrix without causing degradation of physical properties or nullification of the functions of MT-4. The specified dispersing aids for the bonding agent MT-4 were found to be particularly effective to ensure uniform coating of solids in solid propellants employing a hydroxy-terminated polybutadiene binder system while not imparting negative side effects that the dispersing adjuvant of "added" water causes.

Inventors

  • 👤 Marjorie T. Cucksee
  • 👤 Henry C. Allen

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-31 16:41
CPC Classifications
C; C06; C06B; C06B23/00; C06B23/009; C06B21/00; C06B21/0008; C06B21/0025

Claims Analysis

Total Claims: 4
Claim 1
Independent Claim 279 words
In a method relating to processing a solid propellant composition wherein an interfacial bonding agent which is the product prepared by reacting together 2.0 moles of tris 1(2 methylaziridinyl) phosphine oxide, 0.7 mole adipic acid, and 0.3 mole tartaric acid is employed to improve the bond between the binder ingredients of a solid propellant composition comprised of a binder of a hydroxy-terminated polybutadiene, a plasticizer selected from the group consisting of a hydrocarbon processing oil plasticizer, a nonenergetic ester plasticizer, or an energetic ester plasticizer, a diisocyanate curing agent, a burning rate catalyst of Fe 2 O 3 , and an ammonium perchlorate oxidizer blend of 200 micron and 17 micron particle size, the additional improvement to said processing method which enhances the physical and mechanical properties of said propellant composition when cured achieved by incorporating from about 0.01 weight percent to about 0.1 weight percent of said composition a dispersing aid for said interfacial bonding agent selected from a diol having the general formula, R(OH) 2 , wherein R is an alkylene radical, or an iminodiol selected from an iminodiol having the general formula R'N(R"OH) 2 , wherein R' is an aryl or alkyl radical and R" is an alkylene radical, said selected diol or iminodiol being an effective dispersing aid for said interfacial bonding agent which results in improving the efficiency of said interfacial bonding agent by ensuring uniform coating of solids; and said selected diol or iminodiol being reactive to become a part of the binder matrix without causing degradation of the physical and mechanical properties as a result of dewetting or weakening of the bond at the ammonium perchlorate interface of said solid propellant composition.
Claim 2
Dependent Claim 279 words
In a method relating to processing a solid propellant composition wherein an interfacial bonding agent which is the product prepared by reacting together 2.0 moles of tris 1(2 methylaziridinyl) phosphine oxide, 0.7 mole adipic acid, and 0.3 mole tartaric acid is employed to improve the bond between the binder ingredients of a solid propellant composition comprised of a binder of a hydroxy-terminated polybutadiene, a plasticizer selected from the group consisting of a hydrocarbon processing oil plasticizer, a nonenergetic ester plasticizer, or an energetic ester plasticizer, a diisocyanate curing agent, a burning rate catalyst of Fe 2 O 3 , and an ammonium perchlorate oxidizer blend of 200 micron and 17 micron particle size, the additional improvement to said processing method which enhances the physical and mechanical properties of said propellant composition when cured achieved by incorporating from about 0.01 weight percent to about 0.1 weight percent of said composition a dispersing aid for said interfacial bonding agent selected from a diol having the general formula, R(OH) 2 , wherein R is an alkylene radical, or an iminodiol selected from an iminodiol having the general formula R'N(R"OH) 2 , wherein R' is an aryl or alkyl radical and R" is an alkylene radical, said selected diol or iminodiol being an effective dispersing aid for said interfacial bonding agent which results in improving the efficiency of said interfacial bonding agent by ensuring uniform coating of solids; and said selected diol or iminodiol being reactive to become a part of the binder matrix without causing degradation of the physical and mechanical properties as a result of dewetting or weakening of the bond at the ammonium perchlorate interface of said solid propellant composition.
Claim 3
Dependent Claim 64 words
The additional improvement to said processing method as set forth in claim 1 wherein said dispersing aid selected has the general formula R(OH) 2 , wherein said alkylene radical is C 2 H 4 , and wherein said dispersing aid is ethylene glycol which is incorporated in said solid propellant composition in an amount of about 0.03 weight percent of said solid propellant composition.
Claim 4
Dependent Claim 65 words
The additional improvement to said processing method as set forth in claim 1 wherein said dispersing aid selected has the general formula R'N(R"OH) 2 , wherein said alkylene radical is C 2 H 4 , and wherein said dispersing aid is 2,2' benzyl-imino diethanol which is incorporated in said solid propellant composition in an amount of about 0.05 weight percent of said solid propellant composition.

References Cited (Backward Citations)

US3695952A Cited
US3762972A Cited
US3801385A Cited
US3986906A Cited
US3953260A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1981-01-23 1981-07-25 1982-01-24 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1985-01-23 1985-07-25 1986-01-24 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1989-01-23 1989-07-25 1990-01-24 $7700.00 Window Closed / Lapsed

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