SIMULATOR STUDY OF A SATELLITE ATTITUDE CONTROL SYSTEM USING INERTIA WHEELS AND A MAGNET
Automatic attitude control system test for satellite using inertia wheels mounted on air bearings
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Automatic attitude control system test for satellite using inertia wheels mounted on air bearings
Lunar seismograph design and construction, Ranger data analysis equipment installation, and Surveyor project seismograph system testing
Jet condenser heat rejection system tested for flow characteristics
Fuel cell research and technology - plate design, thermal analysis, performance characteristics, water recovery and purity, control techniques, breadboard items, and system test models
Fluid state vortex valve secondary injection control system shows considerable promise for future application to solid propellant rocket engine thrust vector control. The single axis injection system tested would be capable of providing secondary injection thrust vector control using 2000 deg F gas.
Electrical switchgear for space nuclear electrical systems - testing of circuit breakers, engine contractors, and actuators
Performance characteristics of electrochemical cell for oxygen content measurement and removal in sodium test systems
Design of wideband high efficiency optical modulation system tested over 100-MHz band
NRX/EST nuclear rocket test system transfer function measurements by control drum perturbation, and comparison with analysis model predictions
Hydrogen detection calibration system testing and operating procedures
Air-bearing facility for Lunar Orbiter attitude control system testing minimizing external disturbances in platform, platform mass deflection and room thermal currents
Acceptance checkout equipment spacecraft for centralized control and LEM and CSM systems testing
Performance test data for ammonia resistojet attitude control system of stable platform satellites
Mirror and lens testing system using lateral shearing interferometer and gas laser light, interpreting interferograms by digital data processing
Nuclear rocket program status and plans, presenting NERVA reactor and engine system tests
Auxiliary flap system tests using Boeing 367-80 transport aircraft and wind tunnels
Botanical systems tested for effects by lunar soil