Research and development on cells with bellows controlled electrolyte levels progress report no. 3, dec. 10, 1964 - may 10, 1965
Control of electrolyte level in nickel-cadmium cells with metal and plastic bellows
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Control of electrolyte level in nickel-cadmium cells with metal and plastic bellows
Modular concept of operations, manufacturing working plan, management communications, and procedures control for development of Gemini spacecraft
Powdered metal oxide pigments by nucleation for temperature control coatings
Stochastic maximum principle with averaged constraint developed for control problems affected by stochastic process
Space thermal control using fusible materials, with analysis of one-dimensional adiabatic system
Thermionic diode-controlled spacecraft power supply system
Control of electrolyte level in sealed Ni-Cd and Ag-Cd cells with bellows action
Ultraviolet irradiation effects on space stable thermal control zinc coatings
Thermal energy supply improvements to uprate performance of subliming solid control rocket
Performance of vortex valve controlled secondary injection thrust vector system for solid propellant rocket motor control
Development history and design modifications for attitude control subsystem of OGO
Passive temperature and humidity control systems developed for advanced space suits
Conference on mechanical engineering aspects of satellite systems - dynamic structural analyses and developments of control mechanisms, design specifications, and equipment components
Dielectric films used for thermal radiation control coatings
Adaptive filter for estimating system noise inputs from actual residuals developed to control Kalman filter in satellite orbit estimation
General, closed-form, analytical solutions are determined for certain classes of C-minimax control problems, several alternative mathematical theories are derived, and a controller design theory is developed to give optimal control in the presence of unmeasureable external disturbances.
Developing attitude control, orbit adjust, thermal, power, electrical integration, integration test and launch support subsystems for ERTS
Development microprogram control sequence from software system