2004Virtual Community of Pathological Anatomy (University of Castilla La Mancha)Requires access

Low-Cost and Green Solid Propellants for Space Propulsion

L.T. De Luca, Л. Галфетти, F. Severini, Marco Galeotta, R. de Amicis, V. A. Babuk, B. N. Kondrikov, A. B. Vorozhtsov

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Abstract

Ammonium Nitrate (AN), an inorganic solid oxidizer used in rocket propulsion decades ago, produces environmentally friendly combustion products and it is a very cheap energetic material. The main objective of this work is to propose AN-based formulations as good candidates for low cost and green propellant for space exploration. Experiments were performed on several categories of solid compositions: (1) neat AN burning as a solid monopropellant or with minor additives; (2) AN-based metallized propellants; (3) AN+AP (dual oxidizer)-based metallized propellants; and (4) a variety of propellants based on phase-stabilized AN.

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What this paper is about

Ammonium Nitrate (AN), an inorganic solid oxidizer used in rocket propulsion decades ago, produces environmentally friendly combustion products and it is a very cheap energetic material. The main objective of this work is to propose AN-based formulations as good candidates for low cost and green propellant for space exploration. Experiments were performed on several categories of solid compositions: (1) neat AN burning as a solid monopropellant or with minor additives; (2) AN-based metallized propellants; (3) AN+AP (dual oxidizer)-based metallized propellants; and (4) a variety of propellants based on phase-stabilized AN.

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Available abstract

Ammonium Nitrate (AN), an inorganic solid oxidizer used in rocket propulsion decades ago, produces environmentally friendly combustion products and it is a very cheap energetic material. The main objective of this work is to propose AN-based formulations as good candidates for low cost and green propellant for space exploration. Experiments were performed on several categories of solid compositions: (1) neat AN burning as a solid monopropellant or with minor additives; (2) AN-based metallized propellants; (3) AN+AP (dual oxidizer)-based metallized propellants; and (4) a variety of propellants based on phase-stabilized AN.

Key concepts: Propellant, Propulsion, Space (punctuation), Aerospace engineering, Aeronautics, Environmental science, Engineering, Computer science

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