초록 ▼

A processing procedure for incorporating bismuth compounds into isocyanate cured hydroxy terminated binder propellants has been discovered. When added to the propellant formulation in ballistic modifier amounts (.gtoreq.0.25%), bismuth salicylate and bismuth .beta.-resorcylate significantly reduce t

A processing procedure for incorporating bismuth compounds into isocyanate cured hydroxy terminated binder propellants has been discovered. When added to the propellant formulation in ballistic modifier amounts (.gtoreq.0.25%), bismuth salicylate and bismuth .beta.-resorcylate significantly reduce the potlife to less than 1-hour. It was discovered that to maximize propellant potlife the temperature of the mixture at the time of the addition is critically important. The potlife of propellants containing bismuth compounds can be increased to greater than 15 hours at 70.degree. F., when the temperature of the mixture at the addition step for bismuth, is lowered from the normal addition temperature of 150.degree. F., to 60.degree. F. Depending on the formulation and solids loading, the viscosity of the propellant at 60.degree. F. is not greatly affected.

대표청구항 ▼

[ I claim:] [1.] A processing procedure for achieving an extended potlife for isocyanate cured minimum smoke propellants containing bismuth compounds and other ingredients comprising polymers, plasticizer(s), carbon, oxidizer(s), ballistic modifiers, chemical aging stabilizer, curing agent, and cure

[ I claim:] [1.] A processing procedure for achieving an extended potlife for isocyanate cured minimum smoke propellants containing bismuth compounds and other ingredients comprising polymers, plasticizer(s), carbon, oxidizer(s), ballistic modifiers, chemical aging stabilizer, curing agent, and cure catalyst, said processing procedure comprising completing the steps 1-8 as follows:step 1: weigh polymer, plasticizer(s), and carbon and add to mixer preheated to 150.degree. F.;step 2: add oxidizer(s);step 3: mix under vacuum at 150.degree. F. for 2 hours;step 4: cool to 60.degree. F.;step 5: add chemical aging stabilizer, ballistic modifiers, mix under vacuum for 10 minutes;step 6: add curing agent, cure catalyst, and mix an additional 20 minutes;step 7: cast propellant in containers; and,step 8: place container containing propellant in oven at 140.degree. F. for 7 days.