Data return advantages of Earth-Mars-Earth trajectories.
Data return advantages of earth-Mars-earth flyby trajectories over more conventional Mars trajectories
Feitis, P. H.↗
Engineering topics
Feitis, P. H.
Publications and source records attributed to Feitis, P. H..
Optimization of data return from planetary missions by trajectory design.
Data return advantages of earth-Mars-earth flyby trajectories over more conventional Mars trajectories
TRAJECTORY OPTIMIZATION↗
Trajectory design for impulsive Earth-Mars- Earth trajectories launched in 1969 and 1971
Trajectory design and associated computer programs for spacecraft ballistic Earth-Mars round-trip mission
INTERPLANETARY SPACECRAFT↗
Trajectory design for impulsive Earth-Mars- Earth trajectories launched in 1969 and 1971.
Trajectory design for spacecraft which returns in vicinity of earth after Mars encounter analyzed by patched conic model
PLANETARY SPACECRAFT↗
Design Parameters for Ballistic Interplanetary Trajectories. Part II - One-way Transfers to Mercury and Jupiter
Design parameters for ballistic interplanetary trajectories to Mercury and Jupiter
JUPITER /PLANET/↗
Translational and rotational motion of a body entering the Mars atmosphere
Translational and rotational motion of spherical body entering Mars atmosphere - reentry physics
SPHERE↗
Translational and rotational motion of a body entering the martian atmosphere <translations- und rotationsbewegung eines in die marsatmosphaere eintauchenden koerpers<.
Rotational, precessional and nutational motion of body entering Mars atmosphere in vertical and oblique directions
ROTATING SPHERE↗