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- STAR-2 abstract "The STAR-2 Bus is a fully redundant, flight-proven, spacecraft bus designed for geosynchronous missions.It is a satellite platform manufactured by Orbital Sciences Corporation with an apogee kick motor to place a communications satellite into geostationary orbit, a thruster to provide the satellite with orbital station-keeping for a 15 year mission, and solar arrays to provide the satellite payload with 5 kW of electrical power.".
- STAR-2 wikiPageID "14297517".
- STAR-2 wikiPageLength "8170".
- STAR-2 wikiPageOutDegree "23".
- STAR-2 wikiPageRevisionID "663123195".
- STAR-2 wikiPageWikiLink Apogee_kick_motor.
- STAR-2 wikiPageWikiLink Category:Satellite_buses.
- STAR-2 wikiPageWikiLink Communications_satellite.
- STAR-2 wikiPageWikiLink File:OptusD1_SatelliteOnly.jpg.
- STAR-2 wikiPageWikiLink Geostationary_orbit.
- STAR-2 wikiPageWikiLink Horizons-2.
- STAR-2 wikiPageWikiLink Intelsat_11.
- STAR-2 wikiPageWikiLink Intelsat_15.
- STAR-2 wikiPageWikiLink Intelsat_16.
- STAR-2 wikiPageWikiLink Mexsat-3.
- STAR-2 wikiPageWikiLink Mexsat_Bicentenario.
- STAR-2 wikiPageWikiLink Optus_(satellite).
- STAR-2 wikiPageWikiLink Orbital_Sciences_Corporation.
- STAR-2 wikiPageWikiLink Orbital_station-keeping.
- STAR-2 wikiPageWikiLink PanAmSat.
- STAR-2 wikiPageWikiLink Satellite_bus.
- STAR-2 wikiPageWikiLink Solar_panels_on_spacecraft.
- STAR-2 wikiPageWikiLink TELKOM-2.
- STAR-2 wikiPageWikiLink Telkom-2.
- STAR-2 wikiPageWikiLink Thor_5.
- STAR-2 wikiPageWikiLinkText "GEOStar-2".
- STAR-2 wikiPageWikiLinkText "STAR-2".
- STAR-2 hasPhotoCollection STAR-2.
- STAR-2 wikiPageUsesTemplate Template:Reflist.
- STAR-2 subject Category:Satellite_buses.
- STAR-2 hypernym Platform.
- STAR-2 type Company.
- STAR-2 comment "The STAR-2 Bus is a fully redundant, flight-proven, spacecraft bus designed for geosynchronous missions.It is a satellite platform manufactured by Orbital Sciences Corporation with an apogee kick motor to place a communications satellite into geostationary orbit, a thruster to provide the satellite with orbital station-keeping for a 15 year mission, and solar arrays to provide the satellite payload with 5 kW of electrical power.".
- STAR-2 label "STAR-2".
- STAR-2 sameAs m.010fdlzn.
- STAR-2 sameAs Q17083126.
- STAR-2 sameAs Q17083126.
- STAR-2 wasDerivedFrom STAR-2?oldid=663123195.
- STAR-2 isPrimaryTopicOf STAR-2.