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.


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    Title :

    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))


    Contributors:
    A. Pettersson (author) / R. Sanden (author)

    Publication date :

    1995


    Size :

    21 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English