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- W1978775801 abstract "Analysis is made for the possibility of erosion pulsed plasma thruster (PPT) application while solving the task of maintaining the point sustaining a long-operating geostationary artificial Earth satellite. The concept of an erosion PPT with a pulse energy of 200–300 J, designed for holding the attitude of a satellite of 500 kg mass over 10 years is presented. The thruster, with a lifetime of 2–3 × 107 pulses, produces a total pulse of 2.5 × 105 Ns, consuming up to 13 kg of propellant (Teflon). Estimations have shown that the thruster total mass will not exceed 50–60 kg for the flying PPT. Even in the case of a two-fold redundancy the thruster set mass should comprise no more than 0.20-0.25 of the satellite mass. The prospect of a rail design for the PPT discharge chamber with lateral propellant feeding is experimentally examined." @default.
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- W1978775801 date "1995-05-01" @default.
- W1978775801 modified "2023-09-26" @default.
- W1978775801 title "Pulsed plasma thruster of the erosion type for a geostationary artificial Earth satellite" @default.
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- W1978775801 doi "https://doi.org/10.1016/0094-5765(95)00025-u" @default.
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