Web6 aug. 2024 · A drawing of the used thruster is shown in figure 1. It resembles the original design for operation with xenon. For both iodine and adamantane the gas resistance was replaced by a model of larger dimensions. The resistance is used to avoid a discharge in the propellant feeding line. Web12 sep. 2014 · Abstract The plasma plume from a low-power Hall-effect thruster fueled by iodine vapor was characterized with several wetted plasma probes. The plasma source included a laboratory propellant feed system and a laboratory model Hall thruster powered by a breadboard power processing unit. The hollow cathode was fed with xenon.
iSat - Gunter
WebHaving started my career with Scientific research institute in BMSTU, I developed a Hall thruster with xenon and iodine propellant. Continuing to develop as an engineer, I … Web1 jul. 2012 · The performance of a nominal 200 W Hall effect thruster fueled by iodine vapor was evaluated. The system included a laboratory propellant feed system, a flight … cransley bournemouth
A brief review of alternative propellants and requirements for …
WebOther propellants of interest include argon, bismuth, iodine, magnesium, zinc and adamantane. Power levels up to 100 kW have been demonstrated for xenon Hall thrusters. As of 2009 [update] , Hall-effect thrusters … Web24 jan. 2024 · Fig. 11 Plasma density of Hall thrusters versus discharge power 从图11中可以看出,当霍尔推力器功率由1kW增大至10kW,等离子体密度增加约1倍。 等离子体密度升高,离子平均碰撞自由程缩短,放电室内离子碰撞频繁,离子热能化加剧,增加了额外的能量消耗,导致霍尔推力器的推进效率下降,进而影响推力等性能。 WebAn iodine fueled 200 W Busek Hall thruster will fly on NASA's upcoming iSat ( Iodine Satellite) mission. Busek is also preparing a 600 Watt iodine Hall thruster system for … cransley fundraising