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A hand wearable body squeegee comprising a glove portion, a concave squeegee band, and a linear squeegee band.
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| Number | Title | Issue Date |
| 4097317 | Desensitizing agent for compositions containing crystalline high-energy nitrates or nitrites Increasing the stability of composite energetic compositions containing ctalline high-energy nitrates or nitrites by the inclusion of saligenin into the composition.... | 06/27/1978 |
| 4092189 | High rate propellant A method of preparing high burning rate solid propellant grains that have od mechanical properties and the high burning rate solid propellant grains prepared from a multimodal blend of at least one ultra-high burning rate propellant that has been cured an... | 05/30/1978 |
| 4070213 | Dispersing aids for MT-4 Diols of the general formula, R(OH)2, wherein R is an alkylene radic 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° C (1... | 01/24/1978 |
| 4057442 | Method of disposal of pyrotechnic compositions A method for safe, relatively air-pollution free disposal of pyrotechnic compositions is disclosed. High percentage recoveries of the inorganic oxidizer and metallic fuel are achieved, resulting in significant cost benefits, while using a minimum of energ... | 11/08/1977 |
| 4057441 | Solid propellant with burning rate catalyst Finely divided cupric sulfide increases the burning rate, and reduces the pressure exponent of solid propellant compositions.... | 11/08/1977 |
| 4056416 | Radiation polymerized priming compositions Extrudable priming mixture comprising 32-42% normal lead styphnate, 14-16% antimony sulfide, 30-33% barium nitrate, 3.9-4.1% tetracene, 6-8% aluminum powder, and 41/2-8% binder comprising the liquid monomers methyl methacrylate and trimethylolpropanetrime... | 11/01/1977 |
| 4033798 | Complex of nitrocellulose as propellant A solution comprising nitrocellulose and a nitramine consisting of either X (Hexahydro-1,3,5-trinitro-s-triazine), HMX (Octahydro-1,3,5,7-tetranitro-s-tetrazine), or mixtures thereof is dissolved in a volatile, liquid acetate ester, evaporated at room ... | 07/05/1977 |
| 4029529 | Crosslinked carboxyl containing polymer and nitrocellulose as solid propellant binder An energetic binder composition of a carboxy polymer, such as an acrylic ymer, mixed with nitrocellulose and cross-linked with a multifunctional curing agent. A composite type propellant in which the energetic binder is combined with an oxidizer and proc... | 06/14/1977 |
| 4025591 | Bonding explosive fillers with anaerobic curing binders An article of manufacture and a method of producing same is disclosed, wherein the article is a solid explosive composition comprised of a major portion of particulate explosive material bound together by a minor portion of a cured anaerobic binding mater... | 05/24/1977 |
| 4011114 | Cross-linked nitrocellulose propellant formulation 1. A propellant formulation comprising the following ingredients: Nitrocellulose Prepolymer of polyglycoladipate and 2,4-tolylene diisocyanate Nitroglycerin Cyclotetramethylenetetranitramine Aluminum 2-Nitrodiphenylamine. 6. A propellant composition consisting essential... | 03/08/1977 |
| 4000025 | Incorporating ballistic modifiers in slurry cast double base containing compositions Ballistic modifiers of up to one micron in size are slurried and mixed with high impulse propellant slurry in order to produce a high impulse propellant having a plateau or mesa burning characteristic.... | 12/28/1976 |
| 3986910 | Composite propellants containing critical pressure increasing additives Increasing the critical pressure of composite propellants by admixing into he propellant composition an additive selected from the group consisting of (1) oxides of Group II metals, titanium, aluminum, boron, zirconium, and lead; (2) nitrides of Group II m... | 10/19/1976 |
| 3981756 | Process for preparing high density solid propellants High density solid propellants are prepared by a process which comprises mixing the solid propellant components comprising a perfluorinated polymer, such as high molecular weight polytetrafluorethylene, and an inorganic oxidizer salt, such as NF4 | 09/21/1976 |
| 3977923 | Method and solid propellant with unsaturated aziridine cured binder A new class of multiaziridines are provided having the formula: ##EQU1## WHEREIN R1, R2, R3 and R4 are monovalent radicals that may be the same or different and are hydrogen, 1-5 carbon alkyl or 1-5 carbon ... | 08/31/1976 |
| 3972967 | Accelerated curing method for solid propellants A method is disclosed for curing a nitrogen-fluorine propellant in an eleomagnetic alternating field. The propellant is cast into thin walled-titanium tubes of predetermined size and with a graphite-epoxy overwrap. When the propellant-filled tubes are ex... | 08/03/1976 |
| 3963541 | Method of manufacturing reaction mixtures of finely divided metals or alloys and solid perhalogenated carbon compounds A method of manufacturing a mixture of finely divided metals and solid perhalogenated carbon compounds, which mixture is capable of reaction when it is ignited, in which perhalogenated carbon compounds are used as solvents.... | 06/15/1976 |
| 3959042 | High impetus, low flame temperature, composite propellants and method of making High impetus, low flame temperature propellants are produced by the incoration of a polynitramine into a saturated polymer of a lower hydrocarbon.... | 05/25/1976 |
| 3954529 | Flare composition with carboxy functional binder and polyalkylene oxide phosphate ester, and method A flare composition is passivated to prevent gas generation during curing at elevated temperatures by incorporating therein as a passivating agent a small amount of a polyalkylene oxide phosphate ester. The additive also serves to increase the pot life of... | 05/04/1976 |
| 3953260 | Gossypol, an abundant, low-cost iron deactivator, pot-life extender, and processing aid for HTPB propellants In a method wherein propellant ingredients including a hydroxy terminated nder, an isocyanate curative therefor and transition metal compounds or traces thereof are mixed, worked into a suitable container and allowed to cure, gossypol is used to prolong t... | 04/27/1976 |
| 3951706 | Solid propellant mixtures and process of preparation 7. A process for preparing a solid propellant composition having a plateau-burning rate comprising the steps of A. mixing at room temperature the following ingredients until a viscous binder results: B. blending into said binder, until a homogeneous pourable m... | 04/20/1976 |
| 3948698 | Solid propellant compositions having epoxy cured, carboxy-terminated rubber binder Solid propellant compositions wherein the polymeric binder is an all-epoxide cured carboxy-terminated rubber are described. A typical composition contains oxidizer, fuel and a binder formed by curing a carboxy-terminated polybutadiene with a specified mix... | 04/06/1976 |
| 3943208 | Method for binding solid propellant to rocket motor case A method of bonding a solid rocket propellant to a motor casing using a flexible sheet insulant. The flexible sheet insulant is easily installed without intermediate adhesive on the metal or propellant side, retains its self-adhesive properties for long p... | 03/09/1976 |
| 3930844 | Method for disposal of pyrotechnic waste A method for disposing of tracer ammunition pyrotechnic material containing trontium nitrate, magnesium, strontium peroxide, polyvinyl chloride, calcium resinate, barium peroxide, oxamide, zinc stearate, polyethylene, strontium oxalate and lead dioxide, wi... | 01/06/1976 |
