Open AccessTemperature sensitivity of solid heterogeneous rocket propellant AP/HTPB/AI
Author(s) -
B. Florczak
Publication year - 2019
Publication title -
materiały wysokoenergetyczne
Language(s) - English
Resource type - Journals
ISSN - 2083-0165
DOI - 10.22211/matwys/0185
Subject(s) - propellant , ammonium perchlorate , polybutadiene , materials science , solid fuel rocket , rocket (weapon) , rocket propellant , sensitivity (control systems) , composite material , liquid propellant rocket , aluminium , chemical engineering , aerospace engineering , engineering , electronic engineering , copolymer , polymer
The results of research on solid heterogeneous rocket propellant (SHRP) containing: ammonium chlorate(VII) (AP) as an oxidant, a binder based on liquid synthetic rubber, i.e. hydroxylterminated polybutadiene (HTPB), aluminium (Al) and technological additives in a laboratory rocket motor (LRM) are presented to determine the thermal sensitivity of the propellant.