Station keeping for gravity-gradient stabilized satellites
Stationkeeping performance of gravity-gradient stabilization satellite
SEARCH · Engineering Papers
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Stationkeeping performance of gravity-gradient stabilization satellite
Low thrust divergent flow cesium-on-tungsten contact ionization electrostatic thrustor for satellite attitude control and stationkeeping missions
Synchronous orbit stationkeeping techniques, examining thrust control requirements of spin- stabilized spacecraft
Advanced low thrust propulsion systems and propellants evaluation for stationkeeping and stability control of NASA Manned Orbital Research Laboratory
Low thrust divergent flow cesium-on-tungsten contact ionization electrostatic thrustor for satellite attitude control and stationkeeping missions
Performance characteristics of two passive communications satellite configurations using solar radiation for stationkeeping
Structural weight analysis and design charts on feasibility of applying stationkeeping concepts to passive communications satellites
Electrostatic ion thrustor employing cesium on tungsten contact ionization for satellite attitude control and stationkeeping missions
Divergent-flow contact-ionization electrostatic thrustor for satellite attitude control and stationkeeping
Design, development, fabrication, evaluation, and delivery of electrothermal, three axis, spacecraft attitude control and four direction stationkeeping system
Satellite stationkeeping in vicinity of unstable collinear libration points
Solar photovoltaic power systems weight reduction and reliability noting applicability to propulsion, attitude control and stationkeeping missions
Satellite orbit adjustment, stationkeeping and attitude control of typical earth- and sun- synchronous satellites by electric propulsion systems
Electrically heated and radioisotope heated thrusters for satellite attitude control and stationkeeping
Multijet electrothermal systems for attitude control and stationkeeping of synchronous communications satellite
Ammonia resistojet stationkeeping subsystem onboard ATS 4 satellite, noting flight test data agreement with ground tests
Libration point relay satellites for continuous communication link between earth and lunar far side, discussing trajectories and halo orbit stationkeeping
ATS-3 hydrazine orbit control system efficiency evaluation statistical method, considering stationkeeping maneuvers