The present application generally relates to hypergolic hydrocarbon fuel compositions comprising a convenient fuel and a cycloheptatriene and/or its analogs, and methods of making and using the hypergolic hydrocarbon fuel compositions.

The present application generally relates to hypergolic hydrocarbon fuel compositions comprising a convenient fuel and a cycloheptatriene and/or its analogs, and methods of making and using the hypergolic hydrocarbon fuel compositions.

Disclosed is a stabilized solution of 70% to 100% hydrogen peroxide containing an alkali phosphate as a stabilizer, a rocket propellant including a combustible fuel and oxidizer, wherein the oxidizer is a stabilized solution of 70% to 100% hydrogen peroxide, and a rocket having a fuel store, an oxidizer store and a rocket engine, wherein the oxidizer is a stabilized solution of 70% to 100% hydrogen peroxide.

Disclosed is a stabilized solution of 70% to 100% hydrogen peroxide containing an alkali phosphate as a stabilizer, a rocket propellant including a combustible fuel and oxidizer, wherein the oxidizer is a stabilized solution of 70% to 100% hydrogen peroxide, and a rocket having a fuel store, an oxidizer store and a rocket engine, wherein the oxidizer is a stabilized solution of 70% to 100% hydrogen peroxide.

The present disclosure provides for silicon nanoparticles, safety devices, solid propellants, and the like.

The present disclosure provides for silicon nanoparticles, safety devices, solid propellants, and the like.

The present disclosure provides for silicon nanoparticles, safety devices, solid propellants, and the like.

The present disclosure provides for silicon nanoparticles, safety devices, solid propellants, and the like.

The present application generally relates to hypergolic hydrocarbon fuel compositions comprising a convenient fuel and a cycloheptatriene and/or its analogs, and methods of making and using the hypergolic hydrocarbon fuel compositions.

The present disclosure generally pertains to a rocket propulsion oxidizer compound that is a solution, is a homogenous and stable liquid at room temperature and includes nitrous oxide and nitrogen tetroxide. In addition, an apparatus is provided for burning a fuel and nitrous oxide/nitrogen tetroxide. The apparatus has a combustor, a catalyst, a nitrous oxide/nitrogen tetroxide supply passage for directing the nitrous oxide/nitrogen tetroxide to a contact position with the catalyst, and a fuel supply passage for supplying the fuel to the combustor. The catalyst acts to facilitate decomposition of the nitrous oxide/nitrogen tetroxide, while the combustor burns the fuel, the decomposed nitrous oxide/nitrogen tetroxide and/or nitrous oxide/nitrogen tetroxide decomposed in the reaction.