Detail Kajian Teknis Keuntungan Peluncuran Satelit Geostasioner dari Indonesia   Oleh:  Dewi, Sri Rukmini ; Dachlan, T. Zaini Jenis: Article from Bulletin/Magazine Dalam koleksi: Warta Lapan vol. 1 no. 1 (Jan. 1999), page 36-42. Topik: satelit Geostasioner Ketersediaan Perpustakaan Pusat (Semanggi) Nomor Panggil: WW32.1 Non-tandon: 1 (dapat dipinjam: 0) Tandon: tidak ada     Lihat Detail Induk Isi artikel The success of the typical satellite launch and payload operation depend on the quality a quantity of flight path maneuver which extend within a save operating range. The life of satellite in orbit beside of component failure, is limited effectively by the amount of thruster fuel required for “s tion keeping” i.e. maintaining the allocated orbital spot. In other words, when the satellite runs out fuel and electricpower, its life end. Geographical location of launching site effects the quality and the quantity of orbit manew required. Observed from the earth rotation speed and the specific impulse which must be produced change the satellite path from transfer orbit to final orbit, for example the launch of PALAPA B fr Indonesia (Biak island) could increase satellite life 1,5 times more than its launch from Cape Canafe USA. Opini Anda Klik untuk menuliskan opini Anda tentang koleksi ini! Kembali

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