C06B43/00

SOLID COMBUSTIBLE PROPELLANT COMPOSITION
20190169083 · 2019-06-06 ·

A combustible solid propellant composition is disclosed that includes an oxidizer of the reaction product under vacuum of potassium periodate and isocyanate, a polymer binder, a plasticizer, and a fuel.

COMPOSITIONS USABLE AS FLARE COMPOSITIONS, COUNTERMEASURE DEVICES CONTAINING THE FLARE COMPOSITIONS, AND RELATED METHODS
20190169082 · 2019-06-06 ·

A composition that includes a fuel and a perfluoropolyether (PFPE) is disclosed. The composition may be used as a flare composition in a countermeasure device. Countermeasure devices including the flare composition are also disclosed, as are methods of forming grains of the countermeasure device.

COMPOSITIONS USABLE AS FLARE COMPOSITIONS, COUNTERMEASURE DEVICES CONTAINING THE FLARE COMPOSITIONS, AND RELATED METHODS
20190169082 · 2019-06-06 ·

A composition that includes a fuel and a perfluoropolyether (PFPE) is disclosed. The composition may be used as a flare composition in a countermeasure device. Countermeasure devices including the flare composition are also disclosed, as are methods of forming grains of the countermeasure device.

Thruster Propellants

The present invention relates to thruster propellants, processes of making thruster propellants and space vehicles comprising thrusters that employ such propellants. The disclosed thruster propellants are advantageous because do not readily uptake water and are conductive. Furthermore, when compared to previous thruster propellants they have a higher mass, a higher density and/or a lower surface tension. Thus, when used in a thruster, such propellants can generate equal or higher thrust than previous thruster propellants.

Thruster Propellants

The present invention relates to thruster propellants, processes of making thruster propellants and space vehicles comprising thrusters that employ such propellants. The disclosed thruster propellants are advantageous because do not readily uptake water and are conductive. Furthermore, when compared to previous thruster propellants they have a higher mass, a higher density and/or a lower surface tension. Thus, when used in a thruster, such propellants can generate equal or higher thrust than previous thruster propellants.

BISMUTH-BASED ENERGETIC MATERIALS
20190152873 · 2019-05-23 · ·

Energetic compounds based on bismuth salts with reduced toxicity that are obtained through the reaction of soluble bismuth salts with soluble salts of organic or inorganic energetic compounds based on azides, derivatives aromatic nitro compounds or nitrogenous heterocyclic compounds, together with the methods for their preparation and application.

BISMUTH-BASED ENERGETIC MATERIALS
20190152873 · 2019-05-23 · ·

Energetic compounds based on bismuth salts with reduced toxicity that are obtained through the reaction of soluble bismuth salts with soluble salts of organic or inorganic energetic compounds based on azides, derivatives aromatic nitro compounds or nitrogenous heterocyclic compounds, together with the methods for their preparation and application.

PROCESS FOR PROVIDING HEAT TO INDUSTRIAL FACILITIES
20190144273 · 2019-05-16 ·

A process for providing heat to an industrial facility comprises contacting a hydrocarbon fuel with oxygen in a reaction zone under partial oxidation conditions including a below stoichiometric oxygen to fuel molar ratio for full combustion to generate heat in the reaction zone and produce a gaseous effluent stream containing carbon monoxide. At least part of the carbon monoxide from the gaseous effluent stream is converted to one or more of chemical products different from carbon monoxide transferring at least part of the heat generated in reaction zone and/or contained in the gaseous effluent stream is transferred to a separate operation in the industrial facility.

PROCESS FOR PROVIDING HEAT TO INDUSTRIAL FACILITIES
20190144273 · 2019-05-16 ·

A process for providing heat to an industrial facility comprises contacting a hydrocarbon fuel with oxygen in a reaction zone under partial oxidation conditions including a below stoichiometric oxygen to fuel molar ratio for full combustion to generate heat in the reaction zone and produce a gaseous effluent stream containing carbon monoxide. At least part of the carbon monoxide from the gaseous effluent stream is converted to one or more of chemical products different from carbon monoxide transferring at least part of the heat generated in reaction zone and/or contained in the gaseous effluent stream is transferred to a separate operation in the industrial facility.

Fragmenting computer chips

A method comprising bonding a first substrate to a second substrate. The first substrate includes a layer of one or more pairs of reactive material. The method comprising triggering a reaction between the one or more pairs of reactive material and fragmenting the second substrate.