Proceedings, Volume 1; Volume 6

acceleration Aero Propulsion Laboratory AIAA Air Force aircraft airflow airframe airplane applications battery blown BYPASS calibration capability coefficient components compressor stall concept configuration control system cost cycle cyclotron radiation discharge drag dynamic effects efficiency ejector electronic energy exhaust system flight flow-through fuel cell fusion rocket geometry heat heater hydrogen I.W. VICTOR increase increment inlet flow interference drag Ion Thruster Mach number magnetic measurements mission monopropellant motor nacelle NASA neutron nuclear light bulb operating conditions orbit parameters percent performance plasma plug nozzle present pressure ratio problems propellant propulsion system radiation range reactor reference shown in Figure solar array solar cell space spacecraft specific impulse static studies synchronous orbit techniques temperature thermal thermocouple throttle thrust vector thruster transducer transient turbine turbopowered simulators valve vapor vehicle velocity voltage weight wind tunnel wind-on