A Comparative Study of Chemical and Nonchemical Propulsion Systems for Attitude Control and Orbit Correction of Geostationary Satellites of the Type 500 to 1000 Kg. Part a - Statement of the Characteristics of the Systems
1970
78 pages
Report
No indication
English
Unmanned Spacecraft , Propulsion system configurations , Propulsion system performance , Satellite attitude control , Stationary orbits , Chemical propulsion , Electrostatic propulsion , Electrothermal engines , Propulsive efficiency , Radioisotope batteries , Specific impulse , Thrust vector control , NASA subject code 28
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