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Intelsat III F-2 : ウィキペディア英語版 | Intelsat III F-2
Intelsat III F-2 was a communications satellite operated by Intelsat. Launched in 1968 it was operated in geostationary orbit at a longitude of 24 degrees west for around eighteen months.〔 ==Satellite== The second of eight Intelsat III satellites to be launched, Intelsat III F-2 was built by TRW. It was a spacecraft, with its mass reducing to by entry into service as it burned propellant to reach its final orbit. The satellite carried an SVM-2 apogee motor for propulsion and was equipped with two transponders powered by body-mounted solar cells generating 183 watts of power. It was designed for a five-year service life.
抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)』 ■ウィキペディアで「Intelsat III F-2」の詳細全文を読む
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