Follow-on studies and investigation related to the chemical hazards potential study Final report
Safety hazards accompanying use of liquid oxygen and hydrogen aboard spacecraft - cryogenic propellant tank structural analysis
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Safety hazards accompanying use of liquid oxygen and hydrogen aboard spacecraft - cryogenic propellant tank structural analysis
Chemiluminescence of chemical compounds released in upper atmosphere and model of releases leading to upper atmospheric chemi-ionization
Technical feasibility of electric-nuclear propulsion system for manned Mars mission
Remote automatic microscopic system for Mars life detection
Preliminary design of spacecraft configuration and performance analysis of passive attitude control subsystem for gravity gradient stabilized Nimbus satellite
Applications Technology Satellite /ATS/ MISSION - objectives, feasibility, experiment design, and spacecraft description
Application Technology Satellite /ATS/ SPACECRAFT tradeoff and analysis - configuration paraboloid antenna, guidance and control power, spacecraft design, and apogee motor selection
Flight dynamics, experiment operational phase sequence, and support operations for Applications Technology Satellite /ATS/ MISSION
Two-dimensional panel flutter and panel divergence in subsonic flow - wind tunnel testing of two and three-dimensional panels
Spark current flow velocity measurement in hypersonic tracer stream
Hydrogen slush and hydrogen gel systems optimization and vehicle application
Structural stress and deflection and electrical performance analyses of boom antenna configurations for spinning navigation satellite
Deployment methods using parachutes for balloon inflation, and altitude cycling for inflatable buoyant Venus station
Scientific instrumentation for inflatable buoyant Venus station
Performance assessment of attitude control system during coast flight, and of thrust vector control system during powered flight of Voyager spacecraft
Electromagnetic absorption and scattering by contaminants from Apollo spacecraft
Spacecraft configurations and propulsion system module design for Voyager project, based on lunar module descent stage applications
Radio/optical/strapdown inertial guidance systems