Extracted from SPRG source product architecture
Burn rate modifiers are chemical additives used in composite solid rocket propellants to enhance burn rate by reducing the decomposition temperature of the fuel and oxidizer matrix.
SPRG manufactures and supplies lead, copper, and metal-complex based burn-rate systems for propellant development and production programs.
Source reference
BHEF is listed by SPRG as a burn rate modifier for composite solid rocket propellant systems.
DEF is offered as part of SPRG burn rate modifier chemistry for propellant formulation support.
Cupric Salicylate is a copper-based burn rate modifier used in propellant combustion tuning.
M-CBR supports burn-rate tuning in solid propellant systems.
M-LBR is included in SPRG burn-rate modifier portfolio for controlled energetic formulation work.
N-LBR is manufactured for specialist burn-rate modification requirements.
LC-12-15 is listed by SPRG as a burn-rate modifier for defence propulsion chemistry.
Lead Salicylate is a lead-based burn rate modifier used in composite propellant systems.
Lead 2-Ethylhexoate is manufactured as part of SPRG burn rate modifier family.