For one-way transfers between Earth and Mars, charts are obtained that show velocity, time, and angle parameters as functions of eccentricity and semilatus rectum of Sun-focused vehicle conic; for round trips, mission time considered ranges from 130 to 1000 days; set of 22 working charts for Earth-Mars trajectories is made available.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Analysis of trajectory parameters for probe and round-trip missions to Mars


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1960


    Size :

    66 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




    Analysis of trajectory parameters for probe and round-trip missions to venus

    Duga, Jr., J.F. / Simsic, C.R. | Engineering Index Backfile | 1960


    Launch Window Analysis for Round Trip MARS Missions

    J. M. Deerwester / L. A. Manning / B. L. Swenson | NTIS | 1967


    Launch window analysis for round trip Mars missions.

    Deerwester, J. M. / Manning, L. A. / Swenson, B. L. | NTRS | 1968