Solid propellant based on phase-stabilized ammonium nitrate

US5596168A · kind A · utility

Assignee

• Max-Planck-Gesellschaft zur Föderung der Wissenschaften e.V. · US

Inventors

• Klaus Menke · Bruchsal, DE
• Jutta Bohnlein-Mauss · Speyer, DE
• Helmut Schmid · Freudenstadt, DE
• Klaus M. Bucerius · Karlsruhe, DE
• Walther Engel · Edenkoben, DE

Key dates

• Filing date: Sep 29, 1995
• Grant date: Jan 21, 1997
• Expiry date: Sep 29, 2015

Classification

• Technology area (CPC C): Chemistry; Metallurgy
• CPC primary: C06B23/007
• WIPO field: Basic materials chemistry
• WIPO sector: Chemistry

Abstract

A solid propellant for rocket propulsion systems or gas generators compri 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 .mu.m, 15 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/molybdenum oxide in the form of an oxide mixture or mixed oxide.