Low thrust trajectory analyses were used to examine the feasibility of using solar electronic propulsion for Earth escape from a negative C3 launch for deep space missions in order to significantly increase the net delivered mass capability of inexpensive launch vehicles.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Negative C3 Launch Options for Solar System Exploration


    Contributors:
    Leifer, S. (author) / Noca, M. (author)

    Conference:

    Joint Propulsion Conference


    Publication date :

    1998-07-13


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Negative C3 launch for solar system exploration

    Leifer, Stephanie / Noca, Muriel | AIAA | 1998


    Launch Vehicle Options for Exploration

    Collins, D. J. / Canaveral Council of Technical Societies | British Library Conference Proceedings | 2004


    Launch Vehicle Options for Exploration

    Gass, M. / Canaveral Council of Technical Societies | British Library Conference Proceedings | 2004


    System Analysis of Launch Transportation Options for Crew Exploration Vehicle

    Dissel, Adam / Kothari, Ajay / Raghavan, Venkat et al. | AIAA | 2005


    System Analysis of Launch Transportation Options for Crew Exploration Vehicle

    Dissel, A. F. / Kothari, A. P. / Raghavan, V. et al. | British Library Conference Proceedings | 2005