Temperature sensitivity of solid heterogeneous rocket propellant AP/HTPB/AI | Zendy

B. Florczak | Zendy

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Temperature sensitivity of solid heterogeneous rocket propellant AP/HTPB/AI

Author(s) -

B. Florczak

Publication year - 2019

Publication title -

materiały wysokoenergetyczne / high energy materials

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.

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