Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Design of a small H2O2/HTPB hybrid sounding rocket motor


    Contributors:

    Conference:

    34th Aerospace Sciences Meeting and Exhibit ; 1996 ; Reno , NV , U.S.A.



    Publication date :

    1996-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Development of a N2O/HTPB hybrid rocket motor

    Arves, J. / Jones, H. / Kline, K. et al. | AIAA | 1997


    Design of a Lab-scale HP/HTPB Hybrid Rocket Motor

    Kannalath, Rajesh / Kuznetsov, Alexander / Natan, Benveniste | AIAA | 2003


    Design of a N20/HTPB Hybrid Rocket Motor Utilizing a Toroidal Aerospike Nozzle

    Dennis, Jacob / Hernandez, Felipe / Shark, Steven et al. | AIAA | 2010


    Demonstration of 2,500 N-class H2O2/HDPE Hybrid Rocket for Lab-scale Sounding Rocket

    Yun, Yongtae / Jeongmoo, Huh / Kim, Youngil et al. | AIAA | 2018