Accession Number : ADP004439
Title : The Processing of High Viscosity Propellants - Curable and Non Curable,
Corporate Author : MINISTRY OF DEFENCE LONDON (ENGLAND)
Personal Author(s) : Tucker,B. G.
Report Date : 02 JUN 1982
Pagination or Media Count : 9
Abstract : The U.K. has been active for many years with non-cured composite propellant, usually designed plastic propellant. There has also been considerable effort on castable systems which can be subsequently cured. Recently a hybrid type of propellant has been developed, which can be manufactured and extruded in a manner akin to plastic propellant, but cured later. This paper details the production methods used for both types of extrudable propellants. The particular advantages of the propellant are also discussed.
Descriptors : *COMPOSITE PROPELLANTS, *HYBRID PROPELLANTS, *MANUFACTURING, CURING, EXTRUSION, SOLID ROCKET PROPELLANT PLASTICIZERS, SOLID ROCKET PROPELLANT BINDERS, POLYBUTADIENE, ISOPRENE, BUTENES, PLASTICS, RUBBER, HIGH VISCOSITY, METHODOLOGY, QUALITY CONTROL, SOLID ROCKET PROPELLANTS, SYMPOSIA
Distribution Statement : APPROVED FOR PUBLIC RELEASE