Integrated control and airframe development considerations
Integrating space shuttle guidance and control systems with airframe using analytical models, simulation, and laboratory hardware
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Integrating space shuttle guidance and control systems with airframe using analytical models, simulation, and laboratory hardware
Criteria for designing inertial gyroscope systems
Compressibility transformation properties and high speed turbulent boundary layer flow with mass transfer and arbitrary pressure gradient
Space shuttle structural fatigue analysis
OAO thermal subsystem design to provide temperature control for experiments and spacecraft electronic devices
Test facilities and procedures for obtaining aerodynamic data required for studying vehicle-in- tube transportation systems
Display media development and implementation from engineering psychology viewpoint for information transfer in form compatible to sensory-perceptual capabilities
Optimal traction drive system design for lunar roving vehicle, considering weight, energy consumption, operational flexibility, power supply, motor and power train
Wind load aerodynamics effects on launch vehicle flight control systems design
Acrolein photoisomerization in lower excited states, determining fluorescence and phosphorescence quantum yields
Low altitude atmospheric effects on IR beam horizon sensors in carbon dioxide band, noting corrections for spacecraft attitude measurement
Hypervelocity impact damage on complex targets, considering spacecraft and missile design
Orbiting solar telescope design for solar disturbances location and monitoring in H alpha line
Meteorological problems associated with space shuttle design and operations, permitting tradeoff analysis on environment effects
Logistic support reusable earth to orbit space shuttle design, noting weight penalties, payloads and development time
Liquid propellant rocket combustion instability, examining droplet vaporization, wake burning and chemical kinetics
Electric propulsion systems integration into SERT 2 spacecraft, discussing launch imposed environment, thrust vector control, thrustor breakdown, power conditioning, etc
Apollo J mission hardware modification for lunar exploration, describing systems engineering role