Velocity requirements associated with various flight paths to Mars and Venus and resulting propulsion and re-entry weights are combined and varied with other missions system weights which are function of mission goals, trip time and environmental protection; system requirements to determine total mass requirements on Earth orbit are -- propulsion systems for Earth orbit departure, Earth entry systems for different missions, life support systems, navigation and control systems, reconnaissance and scientific instrumentation for gathering data during course of missions, space power supply systems and vehicle design concepts.


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    Title :

    Manned flight to Mars and Venus in 70's


    Additional title:

    AIAA -- Tech Paper


    Contributors:

    Conference:

    Meeting of the 2nd AIAA -- Manned Space Flight ; 1963 Interplanetary



    Publication date :

    1963


    Size :

    18 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :



    MANNED FLIGHT TO MARS AND VENUS IN THE 70'S

    MARTIN, BENJAMIN | AIAA | 1963


    Manned expeditions to Mars and Venus.

    Dixon, F. P. / Gray, E. Z. | NTRS | 1968



    Manned Mars trips using Venus flyby modes

    Sohn, R.L. | Engineering Index Backfile | 1966