초록 ▼

A solid propellant for rocket propulsion systems or gas generators comprises 35 to 80 wt. % ammonium nitrate (AN) in pure or nickel oxide, potassium or cesium nitrate phase-stabilized form (PSAN) with an average particle size of 5 to 200 m

A solid propellant for rocket propulsion systems or gas generators comprises 35 to 80 wt. % ammonium nitrate (AN) in pure or nickel oxide, potassium or cesium nitrate phase-stabilized form (PSAN) with an average particle size of 5 to 200 m

대표청구항 ▼

Solid propellant for rocket propulsion systems or gas generators, comprising 35 to 80 wt. % ammonium nitrate (AN) in pure or nickel oxide, potassium or cesium nitrate phase-stabilized form (PSAN) with an average particle size of 5 to 200 m15 to 50 wt. % of a binder system of a binder polymer and an

Solid propellant for rocket propulsion systems or gas generators, comprising 35 to 80 wt. % ammonium nitrate (AN) in pure or nickel oxide, potassium or cesium nitrate phase-stabilized form (PSAN) with an average particle size of 5 to 200 m15 to 50 wt. % of a binder system of a binder polymer and an energy-rich plasticizer, as well as 0.2 to 5 wt. % of a burning moderator of vanadium oxide/molybdenum oxide as an oxide mixture or mixed oxide.