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

1997-01-21

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

055961681

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.

REFERENCES:
patent: 3340111 (1967-09-01), Stammler
patent: 3609115 (1971-09-01), Sammonds 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.

Affiliated with

Also associated with

Rating

Solid propellant based on phase-stabilized ammonium nitrate does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Solid propellant based on phase-stabilized ammonium nitrate, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Solid propellant based on phase-stabilized ammonium nitrate will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-2325737