Princeton University / International Space Station / /
IndustryTerm
space travel / explicit solutions / energy equation / low energy / interior and exterior low energy transfers / chemical thrusters / inert gas / propulsion systems / energy wrt / planetary dynamical systems / chemical and low-thrust propellant / natural systems / high and low energy transfers / high-energy transfers / spacecraft systems / chemical propulsion / chemical and electric thrusters / dynamical systems / energy savings / thrust propulsion systems / low energy transfer / energy / low-energy transfer / thrust and low-thrust propulsion systems / low energy transfers / excess energy / high-energy transfer / low-thrust propulsion systems / low-energy transfer option space / low-energy transfer trajectory / electric and chemical propulsion / energy transfers / natural dynamical systems / lengthy high-energy transfers / explicit closed form solutions / high energy / less energy / high-energy / chemical and electric propulsion / optimization software / numerical algorithm / low-energy transfers / low energy pathways / wi1h chemical propulsion / low energy trajectories / energy surface / well defined algorithm / low-energy trajectories / transportation system / astronomical dynamic systems / /
OperatingSystem
L3 / /
Organization
Francesco Topputo Aerospace Engineering Department / Princeton University / SMART1 mission / Hiten mission / GRAIL mission / Exploration Platform Integrated mission / National Aeronautics and Space Administration / Politecnico di Milano / Milan / /
Person
Moon Lagrange / Walter Hohmann / Francesco Topputo / /
GLEX[removed]6x12248, Washington, D.C. May 22-24, [removed]EFFICIENT CIS-LUNAR TRAJECTORIES Author: Kevin E. Post Boeing Defense Space & Security, Houston, TX, United States, [removed]