Accession Number : ADD010660

Title :   Solid Rocket Propellants Comprising Guignets Green Pigment.

Descriptive Note : Patent,

Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON DC

Personal Author(s) : Anderson,W S

Report Date : 25 Oct 1983

Pagination or Media Count : 4

Abstract : A solid rocket propellant composition comprising a major amount of ammonium perchlorate, a minor amount of aluminum powder, a minor amount of a binder, and an effective, burn rate modifying amount of Guignet's green pigment or oxidized Guignet's green. Guignet's green pigment increases the burn rate of the propellant without unacceptably increasing the pressure dependence of the burn rate. (Author)

Descriptors :   *Patents, *Solid rocket propellants, *Burning rate, Catalysts, Combustion chambers, Combustion products, Solid propellant rocket engines, Gases, Ammonium perchlorate, Hydroxyl radicals, Polybutadiene, Binders, Inventions

Subject Categories : Information Science
      Combustion and Ignition
      Solid Rocket Propellants

Distribution Statement : APPROVED FOR PUBLIC RELEASE