Nitro-paraffin propellant

Claim 1

A SELF-SUFFICIENT LIQUID PROPELLANT LENDING ITSELF TO USE AS A FUEL IN A GAS TURBINE CONSISTING ESSENTIALLY OF A SELF-CONTAINED STOICHIOMETRIC MIXTURE OF AN OXIDANT SELECTED FROM THE GROUP CONSISTING OF AMMONIUM NITRATE AND AMMONIUM PERCHLORATE AND A FUEL COMPONENT SELECTED FROM THE GROUP CONSISTING OF NITROMETHANE, NITROETHANE, 1-NITROPROPANE, 2-NITROPROPANE, 1,1-DINITROPROPANE, 2,2-DINITROPROPANE, 1,2-DINITROPROPANE, 1,3-DINITROPROPANE, 1,1-DINITROETHANE, TRINITROPROPANE, AND MIXTURES THEREOF, THE PROPELLANT AS A WHOLE TAKING THE PHYSICAL FORM OF A LIQUID DEVOID OF EXTRANEOUS SOLID COMBUSTIBLES IN WHICH THE OXIDANT IS DISPERSED IN FINELY DIVIDED FORM AND WHICH IS SUSCEPTIBLE OF BEING FED IN LIQUID FORM TO THE REGION WHEREIN THE PROPELLANT IS PREPARED FOR BURNING AT THE POINT OF FLAME PROPAGATION IN THE COMBUSTION CHAMBER OF THE TURBINE.