Solid propellant based on phase-stabilized ammonium nitrate

Details Solid propellant based on phase-stabilized ammonium nitrate Solid propellant based on phase-stabilized ammonium nitrate

1995-09-29

1996-12-31

Miller, Edward A.

Explosive and thermic compositions or charges

Structure or arrangement of component or product

Solid particles dispersed in solid solution or matrix

149 191, 149 196, C06B 4510

Patent

active

055896618

ABSTRACT:
5
A solid propellant for rocket propulsion systems or gas generators compri 35 to 80 wt. % ammonium nitrate (AN) with an average particle size of 5 to 200 .mu.m, which is phase-stabilized (PSAN) by chemical reaction with Cu0 or Zn0, 15 to 50 wt. % of a binder system of a binder polymer and an energy-rich plasticizer, as well as 0.2 to 5.0 wt. % of a burning moderator of vanadium/molybdenum oxide as an oxide mixture or mixed oxide.

REFERENCES:
patent: 3340111 (1967-09-01), Stammler
patent: 3609115 (1971-09-01), Sammons et al.
patent: 3629019 (1971-12-01), Lawrence
patent: 3822154 (1974-07-01), Lawrence et al.
patent: 3924405 (1975-12-01), Cohen et al.
patent: 4158583 (1979-06-01), Frosch
patent: 4166045 (1979-08-01), Rudy et al.
patent: 4318270 (1982-03-01), Orlick et al.
patent: 4411717 (1983-10-01), Anderson
patent: 5074938 (1991-12-01), Chi
patent: 5076868 (1991-12-01), Doll et al.
patent: 5292387 (1994-03-01), Highsmith et al.

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