Engine performance parameter, such as thrust, efficiency, specific mass, thruster input, power, thrust-to-power ratio and discharge current have been calculated with specific impulse the indupendent variablel.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Performance Estimate of Large-Scale Ion Engines for SEI-Type Missions Using C(sub 60) Propellant


    Contributors:

    Publication date :

    1993-01-01


    Type of media :

    Preprint


    Type of material :

    No indication


    Language :

    English


    Keywords :




    ADVANCED HIGH ENERGY MATERIALS FOR FUTURISTIC LIQUID PROPELLANT ROCKET ENGINES PROPELLED SPACE MISSIONS

    Malhotra, Vinayak / Ray, Triparna / Velmurugan, Priyadharshini | TIBKAT | 2021


    Manned Mars Missions using Propellant from Space

    Zuppero, A. C. / Olson, T. S. / Redd, L. R. et al. | British Library Conference Proceedings | 1993


    Altitude Testing of Large Liquid Propellant Engines

    B. Maynard / N. Raines | NTIS | 2008