Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Experimental Performance Analysis of a Toroidal Aerospike Nozzle Integrated with a N2O/HTPB Hybrid Rocket Motor


    Contributors:

    Conference:

    46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit



    Publication date :

    2010-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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

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


    DESIGN OF A N~20/HTPB HYBRID ROCKET MOTOR UTILIZING A TOROIDAL AEROSPIKE NOZZLE

    Dennis, J. / Hernandez, F. / Shark, S. et al. | British Library Conference Proceedings | 2010


    NUCLEAR THERMAL ROCKET ENGINE WITH A TOROIDAL AEROSPIKE NOZZLE

    Stewart, Kyle J. / Papadopoulos, Periklis / Pollard, Jordan | TIBKAT | 2020


    Nuclear Thermal Rocket Engine with a Toroidal Aerospike Nozzle

    Stewart, Kyle J. / Papadopoulos, Periklis / Pollard, Jordan | AIAA | 2020