Mariner Venus/Mercury 1973 preliminary mission design
Mission planning for 1973 Mariner Venus/Mercury flyby, discussing trajectory and navigation aspects
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Mission planning for 1973 Mariner Venus/Mercury flyby, discussing trajectory and navigation aspects
Pioneer-F Jupiter flyby mission planning, considering use of optimum broken plane trajectories to increase launch opportunity and/or payload capability
Jupiter swingby trajectory analysis for comet flyby and rendezvous missions, discussing approach velocity and payloads
RF requirements of deep space-outer planet spacecraft communications for Jupiter, Saturn, Uranus and Neptune flyby missions
Automated mission requirements for outer planets, discussing flyby spacecraft, orbiters, atmospheric entry and grand tour missions
The Apollo 13 mission, planned as a lunar landing in the Fra Mauro area, was aborted because of an abrupt loss of service module cryogenic oxygen associated with a fire in one of the two tanks at approximately 56 hours. The lunar module provided the necessary support to sustain a minimum operational condition for a safe return to earth. A circumlunar profile was executed as the most efficient means of earth return, with the lunar module providing power and life support until transfer to the command module just prior to entry. Although the mission was unsuccessful as planned, a lunar flyby and several scientific experiments were completed.
Measuring thermal characteristics of solar arrays for Mariner Venus-Mercury 1973 flyby mission
Computer program for electric propelled spacecraft interplanetary, flyby, and rendezvous trajectory optimization based on Chebyshev approximation and polynomial representations
Planning for Pioneer 5 and 6 interplanetary missions with Jupiter flyby
Preliminary feasibility of depositing atmospheric entry probe from flyby mission to Jupiter
Grand Tour mission design, discussing navigation, trajectory parameters, launch vehicles and satellite flybys
High energy fast Grand Tour multiplanet flyby missions to outer planets omitting Jupiter, noting identical arrival date at Neptune
Ionic and thermal structure model of daytime Venus ionosphere with solar wind heating based on Mariner 5 flyby mission
Mariner 1969 flyby Mars UV spectrum observations, interpreting data in terms of atmospheric, topographic and polar cap adsorptive characteristics
Mission analysis for multi-planet flyby and major satellites close encounter to determine solar system planetary evolution data, presenting Grand Tour trajectory parameters
Outer planet exploration spacecraft subsystems reliability and ten year flight requirements for planet orbiting and flyby missions
Atmospheric entry probe from flyby mission to Jupiter, considering descent trajectory feasibility and instrument package
Trajectory aiming plane in optimum satellite orbit selection for planetary flyby and orbiter missions