The intention of the investigation was to get reference values for judging future aging tests. Static firing at -25 deg C with recording of the thrust was carried out with one rocket motor ARC MARC 133. Laboratory tests were carried out with propellant from another motor and from propellant cast in carton. The laboratory tests contained tensile test, hardness, burning rate, glass transition temperature and adhesion of liner.
Test Number 1 of Propellant for Rocket Motor ARC MARC 133 (Provning Nr 1 av Krut Till Raketmotor ARC MARC 133)
1989
27 pages
Report
No indication
English
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