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    Titel :

    Transient Combustion Response of AP/HTPB Composite Solid Propellant to Acoustic Oscillations in a Rocket Motor



    Kongress:

    Joint meeting; 37th, Joint Army-Navy-NASA-Air Force; Combustion Subcommittee; JANNAF ; 2000 ; Monterey, CA



    Erscheinungsdatum :

    2000-01-01


    Format / Umfang :

    28 pages


    Anmerkungen:

    Held jointly with the 25th Airbreathing Propulsion Subcommittee and the 19th Propulsion Systems Hazards Subcommittee and 1st Modeling and simulation subcommittee meetings


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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