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Advanced Electric Propulsion for Interplanetary Missions
Space Station Propulsion Utilization of Effluents
Multimegawatt Nuclear Power System for Lunar Base Applications
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Advanced aerobraking algorithm alloy American Astronautical Society antenna antiprotons applications Astronautical attitude control Available AAS battery Brayton cycle calculations capability Chair chemical concept configuration control system cost cycle deployable droplet DSMC dynamic electric propulsion electrodynamic tether energy engine equations Figure flight flow fluid frequency fuel gimbal heat horizon sensor laser launch vehicle liquid Mars Mars Observer Martin Marietta Martin Marietta Denver mass mission mode module NASA NASA/HQ nonequilibrium nuclear OCTOBER 28 operation optical output payload performance power system propellant propulsion system radiation reaction wheel reactor reusable rocket rotation Satellite scan platform shield shown in Fig simulation solar sails Space Shuttle Space Station Space Structures spacecraft specific impulse SSTO subsystem surface TECHNICAL SESSION telerobotic temperature tether thermal thrusters Transportation University of Colorado velocity voltage X-band