Two rocket motors ARC-MARC 133 were tested. Static firing at 248K with recording of thrust was carried out with one of the motors. Laboratory tests were carried out with propellant from the other motor and from the same type of propellant cast in carton. The laboratory tests contained tensile test, hardness, burning rate, glass transition temperature and adhesion of the propellant to the liner. The results were compared to results from an earlier testing at FOA.
Aldringskontroll Nr. 2 av Krut i Raketmotor ARC-MARC 133 (RBS 15) (Aging Control No. 2 of Propellants for Rocket Motors ARC-MARC 133 (RBS 15))
1995
21 pages
Report
Keine Angabe
Englisch
Rocket Propellants , Rocket Engines & Motors , Composite rocket propellants , Rocket engines , Aging tests(Materials) , Thermomechanical properties , Propulsion system performance , Service life , Tensile properties , Burning rate , Adhesion tests , Transition temperature , Tensile tests , Thermal expansion , Stress analysis , Glass , Linings , Aging(Materials) , Foreign technology
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