The igniter composition for a solid rocket propellant consists essentially of powdered iron of a major amount by weight and potassium perchlorate.


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    Title :

    Gasless Ignition Composition for Solid Rocket Propellants


    Contributors:

    Publication date :

    1964


    Size :

    1 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





    SOLID ROCKET PROPELLANTS

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    Solid Rocket Propellants

    A. I. Silantev | NTIS | 1967


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    Ho, S. Y. | British Library Conference Proceedings | 1993