The contents of this section contain the initial concepts developed for the In-orbit assembly of a Manned Mars Vehicle and for the Earth-to-Orbit (ETO) delivery of the required hardware and propellant. Two (2) Mars vehicle concepts (all-propulsive and all-aerobrake) and two (2) ET0 Vehicle concepts were investigated. Both Mars Vehicle concepts are described in Reference 1, and both ETO Vehicle concepts are described in Reference 2. The all-aerobrake configuration reduces the number of launches and time required to deliver the necessary hardware/propellent to orbit. Use of the larger of the 2 ETO Vehicles (HLLV) further reduces the number of launches and delivery time; however, this option requires a completely new vehicle and supporting facilities.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Manned Mars Mission Earth-to-Orbit (ETO) Delivery and Orbit Assembly of the Manned Mars Vehicle


    Contributors:
    B Barisa (author) / G Solmon (author)

    Conference:

    Manned Mars Missions Workshop ; 1985 ; Huntsville, AL, US



    Publication date :

    1986-05-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English