Asteroid Belt and Jupiter fly by study First bimonthly progress report
Scientific experiments for asteroid belt study and Jupiter flyby mission
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Scientific experiments for asteroid belt study and Jupiter flyby mission
New linear electron inductive charging apparatus using tungsten filament for voltage amplification
Design and fabrication of sterilization container and model probe assembly for Mars landing capsule
Trajectory and mission analyses for asteroid belt and Jupiter flyby study
Fast scan high resolution mass spectrometer system for use with gas chromatography instrumentation
Comparison of stitched foam thermal insulation protection system for liquid hydrogen tank wall of Centaur launch vehicle with ac-6 jettisonable insulation
Attitude control system optimization as open-loop and stochastic processes for soft landing and antenna pointing problems
Large cadmium sulfide thin film photovoltaic cells
Two-phase heat transfer and fluid flow data for potassium under conditions of boiling and condensing
Metallurgic, thermodynamic, ultrasonic, polymer, and spectroscopic studies in materials science
Solid state physics, plasma physics, and information sciences research activities report
Electron beam melting and welding of tungsten- technetium alloys and density measurements
Magnetic probe and ion collector study of pulsed plasma propulsion system exhaust jet plume
Ion introduction into strong field region of quadropole mass spectrometer
Correlation between porosity defects and mechanical behavior of weld joints
Spacecraft launches and planetary and interplanetary missions to outer planets of solar system
Thermodynamic properties of carbon, hydrogen, oxygen, phosphorus, and sulfur compounds
Systems analysis and integration, boom subsystem, combination passive damper, and attitude sensor system for Applications Technology Satellite gravity gradient stabilization system